A318/A319/A320/A321 31700 BLAGNAC CONF ALL ATA SYSTEM…
Transcript of A318/A319/A320/A321 31700 BLAGNAC CONF ALL ATA SYSTEM…
A318/A319/A320/A321SERVICE BULLETIN
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CONF ALLAIRBUS2, ROND POINT EMILE DEWOITINE31700 BLAGNACFRANCE The content of this document is the property of Airbus.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 informationcontained 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 thecopyright. Requests for reproduction of any data in this document and the media authorized for it mustbe addressed to Airbus.
ATA SYSTEM: 25
TITLE: EQUIPMENT/FURNISHINGS - OVERHEAD STOWAGE COMPARTMENTS -INSPECTION OF OHSC X-FIXATION BRACKETS
MODIFICATION No.:None
A318/A319/A320/A321SERVICE BULLETIN
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TITLE: EQUIPMENT/FURNISHINGS - OVERHEAD STOWAGE COMPARTMENTS -INSPECTION OF OHSC X-FIXATION BRACKETS
SUMMARYThis summary is for information only and is not approved for modification of the aircraft.A. MODIFICATIONS
CONF 001
MODIFICATION CLASSIFICATIONMAJOR NoneMINOR None
NOTE: As per EASA IR 21, a minor change is one that has no appreciable effect on themass, balance, structural strength, reliability, operational characteristics affectingthe airworthiness of the product. All other changes are major changes.
CONF 002
MODIFICATION CLASSIFICATIONMAJOR NoneMINOR None
NOTE: As per EASA IR 21, a minor change is one that has no appreciable effect on themass, balance, structural strength, reliability, operational characteristics affectingthe airworthiness of the product. All other changes are major changes.
CONF ALLB. REASON
(1) HistoryThis Service Bulletin is a result of a Quality Survey Report (QSR) raised when some x-fixation brackets of the Over-Head Stowage Compartment (OHSC) were found missingor installed at 180 deg. in the wrong direction in a production aircraft.
(2) Objective/ActionThis inspection Service Bulletin mandatory to perform a Special Detailed Inspection(SDI) of the x-fixation brackets of the OHSC. Missing brackets shall be installed andbrackets in the incorrect position shall be removed and reinstalled in the correctdirection.
(3) AdvantagesAccomplishment of this Service Bulletin will allow to detect missing or incorrectlyinstalled x-fixation brackets and restore the OHSC to its initial design configuration.
(4) Operational/Maintenance ConsequencesNone
C. GENERAL EVALUATION
EVALUATION TABLECOMPLIANCE RECOMMENDED COST SAVING NO
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SUMMARY
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EVALUATION TABLEA/C OPERATIONAFFECTED
NO VENDOR SB NO
CANCELS INSPECTION SB NO ETOPS AFFECTED NOPAX COMFORT AFFECTED NO POTENTIAL AD YESRELIABILITY AFFECTED NO STRUCTURAL LIFE EXTENSION NOLIFE LIMIT NO LINE MAINTENANCE AFFECTED NO
NOTE: Service Bulletin recommended to be accomplished to prevent significantoperational disruptions.
D. MAINTENANCE CONFIGURATIONCONF 001
No specific aircraft maintenance configuration required.CONF 002
No specific aircraft maintenance configuration required.CONF ALL
E. MATERIAL PRICE INFORMATIONCONF 001
(1) Inspection of the X-Fixation Bracket using an Endoscope Camera(a) Task set A320-A-25-XX-1BQB-01000-93BA-A Inspection of the X-Fixation Bracket
using an Endoscope CameraNo material
(2) Inspection of the X-Fixation Bracket without using Endoscope Camera(Alternative Method)(a) Task set A320-A-25-XX-1BQB-02000-93BA-A Inspection of the X-Fixation Bracket
without using Endoscope Camera (Alternative Method)No material
(3) Repair (Depending on the Inspection Result)(a) Task set A320-A-25-XX-1BQB-01000-93CA-A Repair (Depending on the Inspection
Result)
MATERIAL PRICE INFORMATION TABLE
MATERIAL SET QTYPER A/C PRICE PER A/C MAIN PARTS
Components See SB See Note Bracket, holder, nuts, screws,washers
NOTE: Price information to be obtained from the given supplier.
CONF 002(1) Inspection of the X-Fixation Bracket using an Endoscope Camera
(a) Task set A320-A-25-XX-1BQB-01000-93BA-A Inspection of the X-Fixation Bracketusing an Endoscope CameraNo material
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(2) Inspection of the X-Fixation Bracket without using Endoscope Camera(Alternative Method)(a) Task set A320-A-25-XX-1BQB-02000-93BA-A Inspection of the X-Fixation Bracket
without using Endoscope Camera (Alternative Method)No material
(3) Repair (Depending on the Inspection Result)(a) Task set A320-A-25-XX-1BQB-01000-93CA-A Repair (Depending on the Inspection
Result)
MATERIAL PRICE INFORMATION TABLE
MATERIAL SET QTYPER A/C PRICE PER A/C MAIN PARTS
Components See SB See Note Bracket, holder, nuts, screws,washers
NOTE: Price information to be obtained from the given supplier.
CONF ALLF. APPLICABILITY
This Service Bulletin is applicable to this (these) operator(s):HAL LAN
G. CONCURRENT REQUIREMENTSNone
H. NATURE OF THE WORKCONF 001
(1) Inspection of the X-Fixation Bracket using an Endoscope Camera(a) Task set A320-A-25-XX-1BQB-01000-93BA-A Inspection of the X-Fixation Bracket
using an Endoscope Camera
AIRCRAFT YESEQUIPMENT NO
(2) Inspection of the X-Fixation Bracket without using Endoscope Camera(Alternative Method)(a) Task set A320-A-25-XX-1BQB-02000-93BA-A Inspection of the X-Fixation Bracket
without using Endoscope Camera (Alternative Method)
AIRCRAFT YESEQUIPMENT NO
(3) Repair (Depending on the Inspection Result)(a) Task set A320-A-25-XX-1BQB-01000-93CA-A Repair (Depending on the Inspection
Result)
AIRCRAFT YESEQUIPMENT NO
CONF 002
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(1) Inspection of the X-Fixation Bracket using an Endoscope Camera(a) Task set A320-A-25-XX-1BQB-01000-93BA-A Inspection of the X-Fixation Bracket
using an Endoscope Camera
AIRCRAFT YESEQUIPMENT NO
(2) Inspection of the X-Fixation Bracket without using Endoscope Camera(Alternative Method)(a) Task set A320-A-25-XX-1BQB-02000-93BA-A Inspection of the X-Fixation Bracket
without using Endoscope Camera (Alternative Method)
AIRCRAFT YESEQUIPMENT NO
(3) Repair (Depending on the Inspection Result)(a) Task set A320-A-25-XX-1BQB-01000-93CA-A Repair (Depending on the Inspection
Result)
AIRCRAFT YESEQUIPMENT NO
CONF ALLI. MANPOWER
CONF 001(1) Inspection of the X-Fixation Bracket using an Endoscope Camera
(a) Task set A320-A-25-XX-1BQB-01000-93BA-A Inspection of the X-Fixation Bracketusing an Endoscope Camera
MANPOWERTOTAL MAN-HOURS 3.50 hELAPSED TIME (HOURS) 3.50 h
(2) Inspection of the X-Fixation Bracket without using Endoscope Camera(Alternative Method)(a) Task set A320-A-25-XX-1BQB-02000-93BA-A Inspection of the X-Fixation Bracket
without using Endoscope Camera (Alternative Method)
MANPOWERTOTAL MAN-HOURS 21.50 hELAPSED TIME (HOURS) 9.50 h
(3) Repair (Depending on the Inspection Result)(a) Task set A320-A-25-XX-1BQB-01000-93CA-A Repair (Depending on the Inspection
Result)
MANPOWERTOTAL MAN-HOURS 22.50 hELAPSED TIME (HOURS) 10.50 h
CONF 002
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(1) Inspection of the X-Fixation Bracket using an Endoscope Camera(a) Task set A320-A-25-XX-1BQB-01000-93BA-A Inspection of the X-Fixation Bracket
using an Endoscope Camera
MANPOWERTOTAL MAN-HOURS 4.50 hELAPSED TIME (HOURS) 4.50 h
(2) Inspection of the X-Fixation Bracket without using Endoscope Camera(Alternative Method)(a) Task set A320-A-25-XX-1BQB-02000-93BA-A Inspection of the X-Fixation Bracket
without using Endoscope Camera (Alternative Method)
MANPOWERTOTAL MAN-HOURS 28.50 hELAPSED TIME (HOURS) 12.50 h
(3) Repair (Depending on the Inspection Result)(a) Task set A320-A-25-XX-1BQB-01000-93CA-A Repair (Depending on the Inspection
Result)
MANPOWERTOTAL MAN-HOURS 27.50 hELAPSED TIME (HOURS) 11.50 h
A318/A319/A320/A321SERVICE BULLETIN
SUMMARY
Figure ICN-A320-A-25XX1BQB-A-FAPE3-00YPI-A-002-01 SHEET 1/1REV 00 Sep 18/19 A320-25-1BQBSummary
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CONF ALLJ. GENERAL OVERVIEW
CONF 002
NOTE:
AREA OF INSPECTION
A
A
FR43
FR69
FR43
FR15FWD PAX DOOR
PAX COMPARTMENTEMERGENCY EXIT
PAX COMPARTMENTEMERGENCY EXIT
AFT PAX DOOR
B
- Z230 Z260
B
FR66
FR21
ICN-A320-A-25XX1BQB-A-FAPE3-00YPI-A-002-01
A318/A319/A320/A321SERVICE BULLETIN
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Figure ICN-A320-A-25XX1BQB-A-FAPE3-00YPJ-A-002-01 SHEET 1/1REV 00 Sep 18/19 A320-25-1BQBSummary
Page 8
CONF 001
NOTE:
AREA OF INSPECTION
FR43
FR69
FR43
FR15 FWD PAX DOOR
PAX COMPARTMENTEMERGENCY EXIT
AFT PAX DOORA
B
FR21
B
- Z230 Z260
FR66
A
ICN-A320-A-25XX1BQB-A-FAPE3-00YPJ-A-002-01
A318/A319/A320/A321SERVICE BULLETIN
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ATA SYSTEM: 25
TITLE: EQUIPMENT/FURNISHINGS - OVERHEAD STOWAGE COMPARTMENTS -INSPECTION OF OHSC X-FIXATION BRACKETS
CONF ALL1. PLANNING INFORMATION
A. APPLICABILITY
NOTE: This Service Bulletin is not applicable to aircraft on which MOD No. 162653/K30846(Service Bulletin No. A320–25–1BPY) is embodied.
(1) ModelsON A/C 07844, 07864
320-271NON A/C 07917, 07959
321-271NCONF ALL
(2) Applicability by MSN07844 07864 07917 07959
(3) MSN by configurationCONF 001
MSN CONFIGURATION07844 07864 001
CONF 002
MSN CONFIGURATION07917 07959 002
CONF ALL(4) Configuration definition
CONF 001Configuration 001
CONF 001 is applicable for all A320 New Engine Option (NEO) aircraft given inthe applicability of this Service Bulletin.
CONF 002Configuration 002
CONF 002 is applicable for all A321 New Engine Option (NEO) aircraft given inthe applicability of this Service Bulletin.
CONF ALLB. CONCURRENT REQUIREMENTS
NoneC. REASON
A318/A319/A320/A321SERVICE BULLETIN
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(1) HistoryThis Service Bulletin is a result of a Quality Survey Report (QSR) raised when some x-fixation brackets of the Over-Head Stowage Compartment (OHSC) were found missingor installed at 180 deg. in the wrong direction in a production aircraft.
(2) Objective/ActionThis inspection Service Bulletin mandatory to perform a Special Detailed Inspection(SDI) of the x-fixation brackets of the OHSC. Missing brackets shall be installed andbrackets in the incorrect position shall be removed and reinstalled in the correctdirection.
(3) AdvantagesAccomplishment of this Service Bulletin will allow to detect missing or incorrectlyinstalled x-fixation brackets and restore the OHSC to its initial design configuration.
(4) Operational/Maintenance ConsequencesNone
D. DESCRIPTIONTo accomplish this Service Bulletin it is necessary to:(1) Inspection of the X-Fixation Bracket using an Endoscope Camera
(a) Task set A320-A-25-XX-1BQB-01000-93BA-A Inspection of the X-Fixation Bracketusing an Endoscope Camera
CONF 0011 Do an SDI of the X-fixation Brackets on the LH OHSC using an Endoscope
CameraCONF 002
1 Do an SDI of the X-fixation Brackets on the LH OHSC using an EndoscopeCamera
CONF 0012 Do an SDI of the X-fixation Brackets on the RH OHSC using an Endoscope
CameraCONF 002
2 Do an SDI of the X-fixation Brackets on the RH OHSC using an EndoscopeCamera
CONF ALL(2) Inspection of the X-Fixation Bracket without using Endoscope Camera
(Alternative Method)(a) Task set A320-A-25-XX-1BQB-02000-93BA-A Inspection of the X-Fixation Bracket
without using Endoscope Camera (Alternative Method)CONF 001
1 Do an SDI of the X-fixation Brackets on the LH OHSC without usingEndoscope Camera
CONF 0021 Do an SDI of the X-fixation Brackets on the LH OHSC without using
Endoscope CameraCONF 001
2 Do an SDI of the X-fixation Brackets on the RH OHSC without usingEndoscope Camera
CONF 002
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2 Do an SDI of the X-fixation Brackets on the RH OHSC without usingEndoscope Camera
CONF ALL(3) Repair (Depending on the Inspection Result)
(a) Task set A320-A-25-XX-1BQB-01000-93CA-A Repair (Depending on the InspectionResult)
CONF 0011 Install the Missing X-Fixation Bracket on the LH OHSC Bin Assembly
CONF 0021 Install the Missing X-Fixation Bracket on the LH OHSC Bin Assembly
CONF 0012 Install the Missing X-Fixation Bracket on the RH OHSC Bin Assembly
CONF 0022 Install the Missing X-Fixation Bracket on the RH OHSC Bin Assembly
CONF 0013 Install the Missing X-Fixation Bracket on the LH OHSC Housing Assembly
CONF 0023 Install the Missing X-Fixation Bracket on the LH OHSC Housing Assembly
CONF 0014 Install the Missing X-Fixation Bracket on the RH OHSC Housing Assembly
CONF 0024 Install the Missing X-Fixation Bracket on the RH OHSC Housing Assembly
CONF 0015 Install the Missing X-Fixation Bracket on the Special LH OHSC Bin Assembly
CONF 0025 Install the Missing X-Fixation Bracket on the Special LH OHSC Bin Assembly
CONF 0016 Install the Missing X-Fixation Bracket on the Special RH OHSC Bin Assembly7 Install the Missing X-Fixation Bracket with Fixation Holder on the LH OHSC
Housing AssemblyCONF 002
7 Install the Missing X-Fixation Bracket with Fixation Holder on the LH OHSCHousing Assembly
CONF 0018 Install the Missing X-Fixation Bracket with Fixation Holder on the RH OHSC
Housing Assembly9 Remove and Install the X-Fixation Bracket in the Correct Position on the LH
OHSC Bin AssemblyCONF 002
9 Remove and Install the X-Fixation Bracket in the Correct Position on the LHOHSC Bin Assembly
CONF 00110 Remove and Install the X-Fixation Bracket in the Correct Position on the RH
OHSC Bin AssemblyCONF 002
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10 Remove and Install the X-Fixation Bracket in the Correct Position on the RHOHSC Bin Assembly
CONF 00111 Remove and Install the X-Fixation Bracket in the Correct Position on the LH
OHSC Housing AssemblyCONF 002
11 Remove and Install the X-Fixation Bracket in the Correct Position on the LHOHSC Housing Assembly
CONF 00112 Remove and Install the X-Fixation Bracket in the Correct Position on the RH
OHSC Housing AssemblyCONF 002
12 Remove and Install the X-Fixation Bracket in the Correct Position on the RHOHSC Housing Assembly
CONF 00113 Remove and Install the X-Fixation Bracket in the Correct Position on the
Special LH OHSC Bin AssemblyCONF 002
13 Remove and Install the X-Fixation Bracket in the Correct Position on theSpecial LH OHSC Bin Assembly
CONF 00114 Remove and Install the X-Fixation Bracket in the Correct Position on the
Special RH OHSC Bin Assembly15 Remove and Install the X-Fixation Bracket with Fixation Holder in the
Correct Position on the LH OHSC Housing AssemblyCONF 002
15 Remove and Install the X-Fixation Bracket with Fixation Holder in theCorrect Position on the LH OHSC Housing Assembly
CONF 00116 Remove and Install the X-Fixation Bracket with Fixation Holder in the
Correct Position on the RH OHSC Housing AssemblyCONF ALL
E. COMPLIANCE
(1) ClassificationRECOMMENDED: Service Bulletin recommended to be accomplished to preventsignificant operational disruptions.
(2) Accomplishment TimescaleAccomplishment of this Service Bulletin must be done within 18 months from the issuedate of this Service Bulletin.This Service Bulletin has been classified Recommended. It is expected that anAirworthiness Directive (AD) published by the European Aviation Safety Agency (EASA)will be issued to change this classification to Mandatory. It is anticipated that the ADwill confirm the (thresholds and/or intervals and/or date) given but reference shouldbe made to the AD for confirmation of the mandated accomplishment timescale.
F. APPROVALThe technical content of this document is approved under the authority of DesignOrganisation Approval No. EASA.21J.031.
A318/A319/A320/A321SERVICE BULLETIN
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If an aircraft listed in the applicability has a modification or repair embodied that is notof AIRBUS origin, and which affects the content of this Service Bulletin, the operatoris responsible for obtaining approval by its airworthiness authority for any adaptationnecessary before incorporation of the Service Bulletin.
G. MANPOWERCONF 001
The manpower estimates given in this Service Bulletin are based on the direct labor cost todo 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 notinclude the time to prepare, plan or inspect the work. Manufacture and procurement of partsand tools, drying times for paints, sealants, etc., and general administration work are alsonot included.(1) Inspection of the X-Fixation Bracket using an Endoscope Camera
(a) Task set A320-A-25-XX-1BQB-01000-93BA-A Inspection of the X-Fixation Bracketusing an Endoscope Camera
PREPARATIONJob Set-up 0.25 h
PROCEDUREDo an SDI of the X-fixation Brackets on the LH OHSC usingan Endoscope Camera
1.50 h
Do an SDI of the X-fixation Brackets on the RH OHSC usingan Endoscope Camera
1.50 h
PREPARATION FOR TESTNone
TESTNone
CLOSE-UPClose-up 0.25 h
TOTAL MAN-HOURS 3.50 hELAPSED TIME (HOURS) 3.50 h
NOTE: The minimum man-hours necessary to accomplish this Service Bulletinare those for the Inspection. Depending on the inspection result,additional man-hours can apply.
(2) Inspection of the X-Fixation Bracket without using Endoscope Camera(Alternative Method)(a) Task set A320-A-25-XX-1BQB-02000-93BA-A Inspection of the X-Fixation Bracket
without using Endoscope Camera (Alternative Method)
PREPARATIONJob Set-up 9.00 h
PROCEDUREDo an SDI of the X-fixation Brackets on the LH OHSCwithout using Endoscope Camera
1.50 h
Do an SDI of the X-fixation Brackets on the RH OHSCwithout using Endoscope Camera
1.50 h
PREPARATION FOR TEST
A318/A319/A320/A321SERVICE BULLETIN
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NoneTEST
Testing 0.50 hCLOSE-UP
Close-up 9.00 hTOTAL MAN-HOURS 21.50 hELAPSED TIME (HOURS) 9.50 h
NOTE: For an explanation of the man-hours and elapsed time, refer to theGantt Chart given in Appendix 01.
NOTE: The minimum man-hours necessary to accomplish this Service Bulletinare those for the Inspection. Depending on the inspection result,additional man-hours can apply.
(3) Repair (Depending on the Inspection Result)(a) Task set A320-A-25-XX-1BQB-01000-93CA-A Repair (Depending on the Inspection
Result)
PREPARATIONJob Set-up 9.00 h
PROCEDUREInstall the Missing X-Fixation Bracket on the LH OHSC BinAssembly
0.25 h
Install the Missing X-Fixation Bracket on the RH OHSC BinAssembly
0.25 h
Install the Missing X-Fixation Bracket on the LH OHSCHousing Assembly
0.25 h
Install the Missing X-Fixation Bracket on the RH OHSCHousing Assembly
0.25 h
Install the Missing X-Fixation Bracket on the Special LHOHSC Bin Assembly
0.25 h
Install the Missing X-Fixation Bracket on the Special RHOHSC Bin Assembly
0.25 h
Install the Missing X-Fixation Bracket with Fixation Holderon the LH OHSC Housing Assembly
0.25 h
Install the Missing X-Fixation Bracket with Fixation Holderon the RH OHSC Housing Assembly
0.25 h
Remove and Install the X-Fixation Bracket in the CorrectPosition on the LH OHSC Bin Assembly
0.25 h
Remove and Install the X-Fixation Bracket in the CorrectPosition on the RH OHSC Bin Assembly
0.25 h
Remove and Install the X-Fixation Bracket in the CorrectPosition on the LH OHSC Housing Assembly
0.25 h
Remove and Install the X-Fixation Bracket in the CorrectPosition on the RH OHSC Housing Assembly
0.25 h
Remove and Install the X-Fixation Bracket in the CorrectPosition on the Special LH OHSC Bin Assembly
0.25 h
A318/A319/A320/A321SERVICE BULLETIN
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Remove and Install the X-Fixation Bracket in the CorrectPosition on the Special RH OHSC Bin Assembly
0.25 h
Remove and Install the X-Fixation Bracket with FixationHolder in the Correct Position on the LH OHSC HousingAssembly
0.25 h
Remove and Install the X-Fixation Bracket with FixationHolder in the Correct Position on the RH OHSC HousingAssembly
0.25 h
PREPARATION FOR TESTNone
TESTTesting 0.50 h
CLOSE-UPClose-up 9.00 h
TOTAL MAN-HOURS 22.50 hELAPSED TIME (HOURS) 10.50 h
NOTE: For an explanation of the man-hours and elapsed time, refer to theGantt Chart given in Appendix 01.
CONF 002The manpower estimates given in this Service Bulletin are based on the direct labor cost todo 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 notinclude the time to prepare, plan or inspect the work. Manufacture and procurement of partsand tools, drying times for paints, sealants, etc., and general administration work are alsonot included.(1) Inspection of the X-Fixation Bracket using an Endoscope Camera
(a) Task set A320-A-25-XX-1BQB-01000-93BA-A Inspection of the X-Fixation Bracketusing an Endoscope Camera
PREPARATIONJob Set-up 0.25 h
PROCEDUREDo an SDI of the X-fixation Brackets on the LH OHSC usingan Endoscope Camera
2.00 h
Do an SDI of the X-fixation Brackets on the RH OHSC usingan Endoscope Camera
2.00 h
PREPARATION FOR TESTNone
TESTNone
CLOSE-UPClose-up 0.25 h
TOTAL MAN-HOURS 4.50 hELAPSED TIME (HOURS) 4.50 h
A318/A319/A320/A321SERVICE BULLETIN
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NOTE: The minimum man-hours necessary to accomplish this Service Bulletinare those for the Inspection. Depending on the inspection result,additional man-hours can apply.
(2) Inspection of the X-Fixation Bracket without using Endoscope Camera(Alternative Method)(a) Task set A320-A-25-XX-1BQB-02000-93BA-A Inspection of the X-Fixation Bracket
without using Endoscope Camera (Alternative Method)
PREPARATIONJob Set-up 12.00 h
PROCEDUREDo an SDI of the X-fixation Brackets on the LH OHSCwithout using Endoscope Camera
2.00 h
Do an SDI of the X-fixation Brackets on the RH OHSCwithout using Endoscope Camera
2.00 h
PREPARATION FOR TESTNone
TESTTesting 0.50 h
CLOSE-UPClose-up 12.00 h
TOTAL MAN-HOURS 28.50 hELAPSED TIME (HOURS) 12.50 h
NOTE: For an explanation of the man-hours and elapsed time, refer to theGantt Chart given in Appendix 01.
NOTE: The minimum man-hours necessary to accomplish this Service Bulletinare those for the Inspection. Depending on the inspection result,additional man-hours can apply.
(3) Repair (Depending on the Inspection Result)(a) Task set A320-A-25-XX-1BQB-01000-93CA-A Repair (Depending on the Inspection
Result)
PREPARATIONJob Set-up 12.00 h
PROCEDUREInstall the Missing X-Fixation Bracket on the LH OHSC BinAssembly
0.25 h
Install the Missing X-Fixation Bracket on the RH OHSC BinAssembly
0.25 h
Install the Missing X-Fixation Bracket on the LH OHSCHousing Assembly
0.25 h
Install the Missing X-Fixation Bracket on the RH OHSCHousing Assembly
0.25 h
Install the Missing X-Fixation Bracket on the Special LHOHSC Bin Assembly
0.25 h
A318/A319/A320/A321SERVICE BULLETIN
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Install the Missing X-Fixation Bracket with Fixation Holderon the LH OHSC Housing Assembly
0.25 h
Remove and Install the X-Fixation Bracket in the CorrectPosition on the LH OHSC Bin Assembly
0.25 h
Remove and Install the X-Fixation Bracket in the CorrectPosition on the RH OHSC Bin Assembly
0.25 h
Remove and Install the X-Fixation Bracket in the CorrectPosition on the LH OHSC Housing Assembly
0.25 h
Remove and Install the X-Fixation Bracket in the CorrectPosition on the RH OHSC Housing Assembly
0.25 h
Remove and Install the X-Fixation Bracket in the CorrectPosition on the Special LH OHSC Bin Assembly
0.25 h
Remove and Install the X-Fixation Bracket with FixationHolder in the Correct Position on the LH OHSC HousingAssembly
0.25 h
PREPARATION FOR TESTNone
TESTTesting 0.50 h
CLOSE-UPClose-up 12.00 h
TOTAL MAN-HOURS 27.50 hELAPSED TIME (HOURS) 11.50 h
NOTE: For an explanation of the man-hours and elapsed time, refer to theGantt Chart given in Appendix 01.
CONF ALLH. WEIGHT AND BALANCE
Not changedI. ELECTRICAL LOAD DATA
Not changedJ. REFERENCES
CONF 001(1) Inspection of the X-Fixation Bracket using an Endoscope Camera
(a) Task set A320-A-25-XX-1BQB-01000-93BA-A Inspection of the X-Fixation Bracketusing an Endoscope Camera
AIRCRAFT MAINTENANCE MANUAL (AMM)06-20-00, Page Block 001 06-31-53, Page Block 001Task 12-34-24-869-002
ELECTRICAL STANDARD PRACTICES MANUAL (ESPM)20-55-00
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IN SERVICE INFORMATION (ISI)00.00.00179
NON DESTRUCTIVE TEST MANUAL (NTM)51-90-00
(2) Inspection of the X-Fixation Bracket without using Endoscope Camera(Alternative Method)(a) Task set A320-A-25-XX-1BQB-02000-93BA-A Inspection of the X-Fixation Bracket
without using Endoscope Camera (Alternative Method)
AIRCRAFT MAINTENANCE MANUAL (AMM)06-20-00, Page Block 001 06-31-53, Page Block 001Task 12-34-24-869-002 Task 20-21-11-911-001Task 25-24-00-710-002 Task 25-24-41-000-802
Task 25-24-41-400-802
ELECTRICAL STANDARD PRACTICES MANUAL (ESPM)20-55-00
IN SERVICE INFORMATION (ISI)00.00.00179
NON DESTRUCTIVE TEST MANUAL (NTM)51-90-00
(3) Repair (Depending on the Inspection Result)(a) Task set A320-A-25-XX-1BQB-01000-93CA-A Repair (Depending on the Inspection
Result)
AIRCRAFT MAINTENANCE MANUAL (AMM)06-20-00, Page Block 001 06-31-53, Page Block 001Task 12-34-24-869-002 Task 20-21-11-911-001Task 23-73-45-000-001Task 23-73-45-400-001
Task 25-24-00-710-002
Task 25-24-41-000-802Task 25-24-41-400-802
Task 25-25-11-000-001Task 25-25-11-400-001
ELECTRICAL STANDARD PRACTICES MANUAL (ESPM)20-55-00
STANDARDS MANUAL (SM)CONF 002
(1) Inspection of the X-Fixation Bracket using an Endoscope Camera
A318/A319/A320/A321SERVICE BULLETIN
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(a) Task set A320-A-25-XX-1BQB-01000-93BA-A Inspection of the X-Fixation Bracketusing an Endoscope Camera
AIRCRAFT MAINTENANCE MANUAL (AMM)06-20-00, Page Block 001 06-31-53, Page Block 001Task 12-34-24-869-002
ELECTRICAL STANDARD PRACTICES MANUAL (ESPM)20-55-00
IN SERVICE INFORMATION (ISI)00.00.00179
NON DESTRUCTIVE TEST MANUAL (NTM)51-90-00
(2) Inspection of the X-Fixation Bracket without using Endoscope Camera(Alternative Method)(a) Task set A320-A-25-XX-1BQB-02000-93BA-A Inspection of the X-Fixation Bracket
without using Endoscope Camera (Alternative Method)
AIRCRAFT MAINTENANCE MANUAL (AMM)06-20-00, Page Block 001 06-31-53, Page Block 001Task 12-34-24-869-002 Task 20-21-11-911-001Task 25-24-00-710-002 Task 25-24-41-000-802
Task 25-24-41-400-802
ELECTRICAL STANDARD PRACTICES MANUAL (ESPM)20-55-00
IN SERVICE INFORMATION (ISI)00.00.00179
NON DESTRUCTIVE TEST MANUAL (NTM)51-90-00
(3) Repair (Depending on the Inspection Result)(a) Task set A320-A-25-XX-1BQB-01000-93CA-A Repair (Depending on the Inspection
Result)
AIRCRAFT MAINTENANCE MANUAL (AMM)06-20-00, Page Block 001 06-31-53, Page Block 001Task 12-34-24-869-002 Task 20-21-11-911-001Task 23-73-45-000-001Task 23-73-45-400-001
Task 25-24-00-710-002
Task 25-24-41-000-802Task 25-24-41-400-802
Task 25-25-11-000-001Task 25-25-11-400-001
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ELECTRICAL STANDARD PRACTICES MANUAL (ESPM)20-55-00
STANDARDS MANUAL (SM)CONF ALL
K. PUBLICATION AFFECTEDNone
L. INDUSTRY SUPPORT INFORMATIONAIRBUS will credit the man-hours indicated in this Service Bulletin for inspections that areperformed on aircraft in warranty at the time of such inspection. Credit will be at the agreedin-house warranty labor rate. Claims for labor allowance should be received no later than 90days after completion of the last affected warranted aircraft.For those aircraft in warranty at the time of such inspection with findings further toinspection as per this Service Bulletin:
- AIRBUS will credit the man-hours indicated in this Service Bulletin for correctionsthat are performed on aircraft in warranty at the time of such correction. Credit willbe at the agreed in-house warranty labor rate. Claims for labor allowance should bereceived no later than 90 days after completion of the last affected warranted aircraft.
- AIRBUS will share the costs of accomplishment of this Service Bulletin by crediting theoperator supplied AIRBUS parts for orders placed within 2 years after the initial issuedate of the Service Bulletin. Claims for this allowance should be received no later than90 days after completion of the last affected aircraft of your fleet.
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 retrofitmanagement department: [email protected].
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2. MATERIAL INFORMATIONA. MATERIAL APPLICABILITY
CONF 001Material for task set A320-A-25-XX-1BQB-01000-93BA-A Inspection of the X-Fixation Bracket using an Endoscope Camera
MATERIAL QTY SEE NOTESReferenced tools See SB
Material for task set A320-A-25-XX-1BQB-02000-93BA-A Inspection of the X-Fixation Bracket without using Endoscope Camera (Alternative Method)
MATERIAL QTY SEE NOTESReferenced tools See SB
Material for task set A320-A-25-XX-1BQB-01000-93CA-A Repair (Depending on theInspection Result)
MATERIAL QTY SEE NOTESReferenced tools See SBComponents See SB
CONF 002Material for task set A320-A-25-XX-1BQB-01000-93BA-A Inspection of the X-Fixation Bracket using an Endoscope Camera
MATERIAL QTY SEE NOTESReferenced tools See SB
Material for task set A320-A-25-XX-1BQB-02000-93BA-A Inspection of the X-Fixation Bracket without using Endoscope Camera (Alternative Method)
MATERIAL QTY SEE NOTESReferenced tools See SB
Material for task set A320-A-25-XX-1BQB-01000-93CA-A Repair (Depending on theInspection Result)
MATERIAL QTY SEE NOTESReferenced tools See SBComponents See SB
CONF ALLB. TOOLING
CONF 001Referenced tools for task set A320-A-25-XX-1BQB-01000-93BA-A Inspection of theX-Fixation Bracket using an Endoscope CameraNOTE: To accomplish this Service Bulletin it is necessary to use the tools listed in the
subsequent referenced tasks:Ref. NTM 51-90-00Referenced tools for task set A320-A-25-XX-1BQB-02000-93BA-A Inspection of theX-Fixation Bracket without using Endoscope Camera (Alternative Method)
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NOTE: To accomplish this Service Bulletin it is necessary to use the tools listed in thesubsequent referenced tasks:
Ref. NTM 51-90-00Referenced tools for task set A320-A-25-XX-1BQB-01000-93CA-A Repair(Depending on the Inspection Result)NOTE: To accomplish this Service Bulletin it is necessary to use the tools listed in the
subsequent referenced tasks:Ref. AMM Task 23-73-45-400-001Ref. AMM Task 25-25-11-400-001
CONF 002Referenced tools for task set A320-A-25-XX-1BQB-01000-93BA-A Inspection of theX-Fixation Bracket using an Endoscope CameraNOTE: To accomplish this Service Bulletin it is necessary to use the tools listed in the
subsequent referenced tasks:Ref. NTM 51-90-00Referenced tools for task set A320-A-25-XX-1BQB-02000-93BA-A Inspection of theX-Fixation Bracket without using Endoscope Camera (Alternative Method)NOTE: To accomplish this Service Bulletin it is necessary to use the tools listed in the
subsequent referenced tasks:Ref. NTM 51-90-00Referenced tools for task set A320-A-25-XX-1BQB-01000-93CA-A Repair(Depending on the Inspection Result)NOTE: To accomplish this Service Bulletin it is necessary to use the tools listed in the
subsequent referenced tasks:Ref. AMM Task 23-73-45-400-001Ref. AMM Task 25-25-11-400-001
CONF ALLC. CONSUMABLES
No consumablesD. LIST OF NEW PARTS
CONF 001Components for task set A320-A-25-XX-1BQB-01000-93CA-A Repair (Depending onthe Inspection Result)
Procurement address D4296
AIRBUS Material, Logistics and SuppliersCustomer Order FulfilmentWeg beim Jaeger 150D-22335 HAMBURGGERMANYPhone: +49 (0) 40 50 76 40 02E-mail: Please contact your Single Point Of Contact(SPOC)Internet: http://spares.airbus.com
NOTE(S)
A318/A319/A320/A321SERVICE BULLETIN
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Customers with aircraft shown in the applicability of this Service Bulletin should senda purchase order to AIRBUS at the address given above and quote the number of thisService Bulletin.Operator supplied AIRBUS parts required to accomplish this Service Bulletin are to bepurchased by a spares purchase order.
ITEM PART No. QTY (UM) KEYWORD DRAWING SEE NOTES
1 606A00305-000(D4296) 2 BRACKET (1) (2)
2 606A00305-001(D4296) 2 BRACKET (1) (2)
3 606A00305-004(D4296) 1 BRACKET (1) (2)
4 606A00305-005(D4296) 1 BRACKET (1) (2)
6 NAS1801-08-5(D4296) 8 SCREW (1) (2)
7 NAS1149CN832R(D4296) 24 WASHER (1) (2)
8 NAS1801-08-10(D4296) 8 SCREW (1) (2)
9 NAS1801-08-7(D4296) 8 SCREW (1) (2)
10 MS21042-08 (D4296) 8 NUT (1) (2)
11 606A00095-002(D4296) 2 HOLDER (1) (2)
NOTE(S)Refer to the AIRBUS Ref. SM if you find part numbers of hardware components whichyou cannot identify. The SM will give you the correct part number to part numberrelationship.
(1): The components listed above are only necessary if Ref. Task set A320-A-25-XX-1BQB-01ZZZ-93CZ-A is to be accomplished. The quantity of these items are to beordered as required.
(2): The components listed above are not an AIRBUS Kit, the required parts must beordered as necessary through the given channel.
CONF 002Components for task set A320-A-25-XX-1BQB-01000-93CA-A Repair (Depending onthe Inspection Result)
Procurement address D4296
AIRBUS Material, Logistics and SuppliersCustomer Order FulfilmentWeg beim Jaeger 150D-22335 HAMBURGGERMANYPhone: +49 (0) 40 50 76 40 02E-mail: Please contact your Single Point Of Contact(SPOC)Internet: http://spares.airbus.com
NOTE(S)
A318/A319/A320/A321SERVICE BULLETIN
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Customers with aircraft shown in the applicability of this Service Bulletin should senda purchase order to AIRBUS at the address given above and quote the number of thisService Bulletin.Operator supplied AIRBUS parts required to accomplish this Service Bulletin are to bepurchased by a spares purchase order.
ITEM PART No. QTY (UM) KEYWORD DRAWING SEE NOTES
1 606A00305-000(D4296) 2 BRACKET (1) (2)
2 606A00305-001(D4296) 1 BRACKET (1) (2)
3 606A00305-004(D4296) 1 BRACKET (1) (2)
6 NAS1801-08-5(D4296) 8 SCREW (1) (2)
7 NAS1149CN832R(D4296) 16 WASHER (1) (2)
8 NAS1801-08-10(D4296) 4 SCREW (1) (2)
9 NAS1801-08-7(D4296) 4 SCREW (1) (2)
10 MS21042-08 (D4296) 4 NUT (1) (2)
11 606A00095-002(D4296) 1 HOLDER (1) (2)
NOTE(S)Refer to the AIRBUS Ref. SM if you find part numbers of hardware components whichyou cannot identify. The SM will give you the correct part number to part numberrelationship.
(1): The components listed above are only necessary if Ref. Task set A320-A-25-XX-1BQB-01ZZZ-93CZ-A is to be accomplished. The quantity of these items are to beordered as required.
(2): The components listed above are not an AIRBUS Kit, the required parts must beordered as necessary through the given channel.
CONF ALLE. LIST OF EXISTING PARTS
No parts
A318/A319/A320/A321SERVICE BULLETIN
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3. ACCOMPLISHMENT INSTRUCTIONSTask set A320-A-25-XX-1BQB-01000-93BA-AInspection of the X-Fixation Bracket using an Endoscope Camera
WARNING: MAKE SURE THAT YOU OBEY ALL THE WARNINGS AND ALL THE CAUTIONSINCLUDED IN THE REFERENCED PROCEDURES.
CAUTION: ALWAYS OBEY THE PRECAUTIONS THAT FOLLOW TO KEEP ELECTRICALWIRING IN A SATISFACTORY CONDITION (ELECTRICALLY AND MECHANICALLYSERVICEABLE). WHEN YOU DO MAINTENANCE WORK, REPAIRS ORMODIFICATIONS, ALWAYS KEEP ELECTRICAL WIRING, COMPONENTS ANDTHE 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 ANDDAMAGE 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 inother 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 thisService 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 stepsto add flexibility to their maintenance operations as long as the technical intent of theService Bulletin is met within the set parameters.
NOTE: Manual titles given in the accomplishment instructions are referred to by acronyms. Referto paragraph 1.J., References, for the definition of acronyms.
NOTE: The purpose of flowcharts is to supplement the information given in the Procedure andCompliance paragraphs and not to serve as the primary source for tasks or compliancetimes given in this Service Bulletin.
NOTE: This Service Bulletin is classified mandatory or expected to be classified mandatory byan Airworthiness Directive (AD). The paragraphs 3.C. and 3.E. in these accomplishmentinstructions 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 theseparagraphs 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 givenin the Service Bulletin, as long as the RC paragraphs can be done and the aircraft can beput back into a serviceable condition.
NOTE: This Service Bulletin contains the instructions for the on-aircraft maintenance necessaryto ensure the continued airworthiness of the aircraft.For any deviations to the instructions, including RC paragraph contained herein, contactAIRBUS for further instructions and approval.
A. TASK SET ASSOCIATED INFORMATIONTask Manpower
CONF 001TOTAL MAN-HOURS 3.50 h
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CONF 002TOTAL MAN-HOURS 4.50 h
CONF 001ELAPSED TIME (HOURS) 3.50 h
CONF 002ELAPSED TIME (HOURS) 4.50 h
CONF ALLB. PREPARATION
(1) Task A320-A-25-XX-1BQB-01001-540A-A - Job Set-upJob Set-Up Information
Manpower/Resources/Skills
Man-hours 0.25 hMinimum Number of person 1Elapsed Time 0.25 h
Referenced Information
Manuals/Drawings References/SheetsAMM Task 12-34-24-869-002
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 Task12-34-24-869-002.
C. PROCEDURECONF 001
(1) Task A320-A-25-XX-1BQB-01001-312A-A - Do an SDI of the X-fixationBrackets on the LH OHSC using an Endoscope CameraJob Set-Up Information
Working Area
Impacted Zone Access / Work Location230 Work location From Frame 21 to Frame 35240 Work location From Frame 35 to Frame 47250 Work location From Frame 47 to Frame 64260 Work location From Frame 64 to Frame 66
Manpower/Resources/Skills
Man-hours 1.50 hMinimum Number of person 1Elapsed Time 1.50 hSkills Cabin
Referenced Information
Manuals/Drawings References/SheetsAMM 06-20-00, Page Block 001
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Manuals/Drawings References/Sheets06-31-53, Page Block 001
ISI 00.00.00179NTM 51-90-00
Procedure(a) Standard Practices
1 For the identification of zones, refer to Ref. AMM 06-20-00, Page Block 001.2 For the Frame (FR) identification, refer to Ref. AMM 06-31-53, Page Block
001.(b) Identify the applicable LH OHSC PNs on the ID label of the OHSC which is located
behind the light cover to do the SDI.Refer to Ref. Fig. Location and Identification of the LH Over-Head StowageCompartment Part Numbers.
(c) Do an SDI of the x-fixation brackets using an endoscope camera insertedbetween the OHSC bin assembly and the filler panel, refer to Ref. NTM 51-90-00.Refer to Ref. Fig. Inspection of the LH Over-Head Stowage Compartment X-Fixation Brackets and Ref. Fig. Flowchart.1 If an x-fixation bracket is found missing, install the bracket in accordance
with:Ref. Task A320-A-25-XX-1BQB-01ZZZ-600Z-AorRef. Task A320-A-25-XX-1BQB-03ZZZ-600Z-AorRef. Task A320-A-25-XX-1BQB-05ZZZ-600Z-AorRef. Task A320-A-25-XX-1BQB-07ZZZ-600Z-A
2 If an x-fixation bracket is found installed incorrectly, remove and install thebracket correctly in accordance with:Ref. Task A320-A-25-XX-1BQB-09ZZZ-600Z-AorRef. Task A320-A-25-XX-1BQB-11ZZZ-600Z-AorRef. Task A320-A-25-XX-1BQB-13ZZZ-600Z-AorRef. Task A320-A-25-XX-1BQB-15ZZZ-600Z-A
NOTE: The x-fixation brackets are installed in ‘Flight Direction’ on thefront side of the housing and bin.
3 Complete the Inspection Report Sheet, refer to Ref. Fig. Inspection report.4 Send the completed Inspection Report sheet in accordance with Ref. ISI
00.00.00179.
NOTE: To send the Inspection Report sheet is not Required for Compliance(RC).
5 If the x-fixation brackets are found installed correctly, no further action isnecessary.
A318/A319/A320/A321SERVICE BULLETIN
Figure ICN-A320-A-25XX1BQB-A-FAPE3-01DLM-A-001-01 SHEET 1/3REV 00 Sep 18/19 A320-25-1BQBLocation and Identification of the LH Over-
Head Stowage Compartment Part Numbers Page 28
CONF 001
FR43
FR69
FR43
FR15
C
C
C
C
C
C
C
C
C
CFWD PAX DOOR
PAX COMPARTMENTEMERGENCY EXIT
AFT PAX DOOR
NOTE:REFER TO SHEET 03, TABLE 01.01
A 01
01B
A
B
C
D
E
F
G
H
J
K
L
FR21
B
- Z230 Z260
FR66
C
A
ICN-A320-A-25XX1BQB-A-FAPE3-01DLM-A-001-01
A318/A319/A320/A321SERVICE BULLETIN
Figure ICN-A320-A-25XX1BQB-A-FAPE3-01DLN-A-001-01 SHEET 2/3REV 00 Sep 18/19 A320-25-1BQBLocation and Identification of the LH Over-
Head Stowage Compartment Part Numbers Page 29
CONF 001
ID-LABEL
LIGHTCOVER
BIN ASSEMBLY
FILLER PANEL
HOUSING
X-FIXATIONBRACKET
CTYPICAL
VIEW LOOKING FWD
INBD
ICN-A320-A-25XX1BQB-A-FAPE3-01DLN-A-001-01
A318/A319/A320/A321SERVICE BULLETIN
Figure ICN-A320-A-25XX1BQB-A-FAPE3-01DLO-A-001-01 SHEET 3/3REV 00 Sep 18/19 A320-25-1BQBLocation and Identification of the LH Over-
Head Stowage Compartment Part Numbers Page 30
CONF 001
A 1 E2529400000000 4 FR LH OHSC
B 1 E2529400200800 4 FR LH OHSC
C 1 E2529400400200 4 FR LH OHSC
D 1 E2529400600200 4 FR LH OHSC
E 1 E2529402400000 4 FR LH OHSC
F 1 E2529401000200 4 FR LH OHSC
G 1 E2529401200200 4 FR LH OHSC
H 1 E2529401400400 4 FR LH OHSC
J 1 E2529401600400 4 FR LH OHSC
K 1 E2529401800000 4 FR LH OHSC
L 1 E2529404801000 3 FR LH OHSC
POSITION QUANTITY PART NUMBER OHSC VARIANT
TABLE 01
ICN-A320-A-25XX1BQB-A-FAPE3-01DLO-A-001-01
A318/A319/A320/A321SERVICE BULLETIN
Figure ICN-A320-A-25XX1BQB-A-FAPE3-00Y3B-A-003-01 SHEET 1/2REV 00 Sep 18/19 A320-25-1BQBInspection of the LH Over-Head Stowage
Compartment X-Fixation Brackets Page 31
CONF 001
FR43
FR69
FR43
FR15
C
C
C
C
C
C
C
C
C
CFWD PAX DOOR
PAX COMPARTMENTEMERGENCY EXIT
AFT PAX DOORA
B
FR21
B
- Z230 Z260
FR66
C
A
ICN-A320-A-25XX1BQB-A-FAPE3-00Y3B-A-003-01
A318/A319/A320/A321SERVICE BULLETIN
Figure ICN-A320-A-25XX1BQB-A-FAPE3-00Y3C-A-002-01 SHEET 2/2REV 00 Sep 18/19 A320-25-1BQBInspection of the LH Over-Head Stowage
Compartment X-Fixation Brackets Page 32
CONF 001
ID-LABEL
LIGHTCOVER
BIN ASSEMBLY
ENDOSCOPECAMERA
FILLER PANEL
HOUSING
X-FIXATIONBRACKET
CTYPICAL
VIEW LOOKING FWD
INBD
BIN ASSEMBLY
HOUSING
D
X-FIXATIONBRACKETS
DNOTE:
CAMERA VIEW.01
01
ICN-A320-A-25XX1BQB-A-FAPE3-00Y3C-A-002-01
A318/A319/A320/A321SERVICE BULLETIN
Figure ICN-A320-A-25XX1BQB-A-FAPE3-00YPG-A-009-01 SHEET 1/1REV 00 Sep 18/19 A320-25-1BQBFlowchart
Page 33
CONF 001
YES
E2529400000000, E2529400200800, E2529400400200, E2529400600200, E2529401000200, E2529401200200, E2529401400400, E2529401600400, E2529401800000, E2529402400000, E2529404801000
DO AN INSPECTION OF LH OHSC LISTED BELOW:
THE PURPOSE OF FLOWCHARTS IS TO SUPPLEMENT THE INFORMATIONGIVEN IN THE PROCEDURE AND COMPLIANCE PARAGRAPHS AND NOT TOSERVE AS THE PRIMARY SOURCE FOR TASKS OR COMPLIANCE TIMESGIVEN IN THIS SERVICE BULLETIN.
NO
SEND THE COMPLETEDINSPECTION REPORT SHEET
INSTALLED
IS ANX-FIXATION BRACKET
INCORRECTLY?
NOYESFOUND
IS ANX-FIXATION BRACKET
MISSING?
INSTALL THE X-FIXATION BRACKET
INSTALL THE X-FIXATION BRACKET
NOTE:FOR THE ACCOMPLISHMENT TIMESCALE, REFER TO PARAGRAPH 1.E.(2).01
01
NO FURTHER ACTIONWITH THIS SERVICE
BULLETIN
ICN-A320-A-25XX1BQB-A-FAPE3-00YPG-A-009-01
A318/A319/A320/A321SERVICE BULLETIN
Figure ICN-A320-A-25XX1BQB-A-FAPE3-01IGW-A-001-01 SHEET 1/1REV 00 Sep 18/19 A320-25-1BQBInspection report
Page 34
CONF 001
INSPECTION REPORT
SERVICE BULLETIN No:
A/C MSN :
FLIGHT CYCLES (FC):
FLIGHT HOURS (FH):
A320-25-1BQB
DATE OF INSPECTION:
SEND THE COMPLETED INSPECTION REPORTSHEET IN ACCORDANCE WITH ISI 00.00.00179
INSPECTION METHOD: SPECIAL DETAILEDINSPECTION (SDI)
SDI OF OHSC X-FIXATION BRACKET
PART NUMBER (PN) CHECK OF THE LH OHSC
AFFECTED OHSC PN;
BRACKET NOT INSTALLED:
BRACKET INSTALLED INCORRECTLY:
ICN-A320-A-25XX1BQB-A-FAPE3-01IGW-A-001-01
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CONF 002(1) Task A320-A-25-XX-1BQB-01002-312A-A - Do an SDI of the X-fixation
Brackets on the LH OHSC using an Endoscope CameraJob Set-Up Information
Working Area
Impacted Zone Access / Work Location230 Work location From Frame 21 to Frame 35.8240 Work location From Frame 35.8 to Frame 47250 Work location From Frame 47 to Frame 64260 Work location From Frame 64 to Frame 66
Manpower/Resources/Skills
Man-hours 2.00 hMinimum Number of person 1Elapsed Time 2.00 hSkills Cabin
Referenced Information
Manuals/Drawings References/Sheets
AMM 06-20-00, Page Block 00106-31-53, Page Block 001
ISI 00.00.00179NTM 51-90-00
Procedure(a) Standard Practices
1 For the identification of zones, refer to Ref. AMM 06-20-00, Page Block 001.2 For the Frame (FR) identification, refer to Ref. AMM 06-31-53, Page Block
001.(b) Identify the applicable LH OHSC PNs on the ID label of the OHSC which is located
behind the light cover to do the SDI.Refer to Ref. Fig. Location and Identification of the LH Over-Head StowageCompartment Part Numbers.
(c) Do an SDI of the x-fixation brackets using an endoscope camera insertedbetween the OHSC bin assembly and the filler panel, refer to Ref. NTM 51-90-00.Refer to Ref. Fig. Inspection of the LH Over-Head Stowage Compartment X-Fixation Brackets and Ref. Fig. Flowchart.1 If an x-fixation bracket is found missing, install the bracket in accordance
with:Ref. Task A320-A-25-XX-1BQB-01ZZZ-600Z-AorRef. Task A320-A-25-XX-1BQB-03ZZZ-600Z-AorRef. Task A320-A-25-XX-1BQB-05ZZZ-600Z-AorRef. Task A320-A-25-XX-1BQB-07ZZZ-600Z-A
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REV 00 Sep 18/19 A320-25-1BQBPage 36
2 If an x-fixation bracket is found installed incorrectly, remove and install thebracket correctly in accordance with:Ref. Task A320-A-25-XX-1BQB-09ZZZ-600Z-AorRef. Task A320-A-25-XX-1BQB-11ZZZ-600Z-AorRef. Task A320-A-25-XX-1BQB-13ZZZ-600Z-AorRef. Task A320-A-25-XX-1BQB-15ZZZ-600Z-A
NOTE: The x-fixation brackets are installed in ‘Flight Direction’ on thefront side of the housing and bin.
3 Complete the Inspection Report Sheet, refer to Ref. Fig. Inspection report.4 Send the completed Inspection Report sheet in accordance with Ref. ISI
00.00.00179.
NOTE: To send the Inspection Report sheet is not Required for Compliance(RC).
5 If the x-fixation brackets are found installed correctly, no further action isnecessary.
A318/A319/A320/A321SERVICE BULLETIN
Figure ICN-A320-A-25XX1BQB-A-FAPE3-01DLS-A-001-01 SHEET 1/3REV 00 Sep 18/19 A320-25-1BQBLocation and Identification of the LH Over-
Head Stowage Compartment Part Numbers Page 37
CONF 002
A
NOTE:REFER TO SHEET 03, TABLE 01.01
A 01
FR43
FR69
FR43
FR15FWD PAX DOOR
PAX COMPARTMENTEMERGENCY EXIT
PAX COMPARTMENTEMERGENCY EXIT
AFT PAX DOOR
01B
C
C
C
C
C
C
C
C
C
A
B
C
D
EF
G
H
J
KL
M
N
P
Q
- Z230 Z260
B
C
FR66
FR21
CC
C
C
C
C
ICN-A320-A-25XX1BQB-A-FAPE3-01DLS-A-001-01
A318/A319/A320/A321SERVICE BULLETIN
Figure ICN-A320-A-25XX1BQB-A-FAPE3-01DLT-A-001-01 SHEET 2/3REV 00 Sep 18/19 A320-25-1BQBLocation and Identification of the LH Over-
Head Stowage Compartment Part Numbers Page 38
CONF 002
ID-LABEL
LIGHTCOVER
BIN ASSEMBLY
FILLER PANEL
HOUSING
X-FIXATIONBRACKET
CTYPICAL
VIEW LOOKING FWD
INBD
ICN-A320-A-25XX1BQB-A-FAPE3-01DLT-A-001-01
A318/A319/A320/A321SERVICE BULLETIN
Figure ICN-A320-A-25XX1BQB-A-FAPE3-01DLU-A-001-01 SHEET 3/3REV 00 Sep 18/19 A320-25-1BQBLocation and Identification of the LH Over-
Head Stowage Compartment Part Numbers Page 39
CONF 002
A 1 E2529408800200 2 FR LH OHSC
B 1 E2529400200600 4 FR LH OHSC
C 1 E2529402000600 4 FR LH OHSC
D 1 E2529405200600 2 FR LH OHSC
E 1 E2529405600200 2 FR LH OHSC
F 1 E2529405800600 2 FR LH OHSC
G 1 E2529402200800 4 FR LH OHSC
H 1 E2529402400200 4 FR LH OHSC
J 1 E2529402600600 4 FR LH OHSC
K 1 E2529406800200 1 FR LH OHSC
L 1 E2529402800600 4 FR LH OHSC
M 1 E2529401400600 4 FR LH OHSC
N 1 E2529401600600 4 FR LH OHSC
P 1 E2529401800200 4 FR LH OHSC
Q 1 E2529404800800 3 FR LH OHSC
POSITION QUANTITY PART NUMBER OHSC VARIANT
TABLE 01
ICN-A320-A-25XX1BQB-A-FAPE3-01DLU-A-001-01
A318/A319/A320/A321SERVICE BULLETIN
Figure ICN-A320-A-25XX1BQB-A-FAPE3-00Y3H-A-003-01 SHEET 1/2REV 00 Sep 18/19 A320-25-1BQBInspection of the LH Over-Head Stowage
Compartment X-Fixation Brackets Page 40
CONF 002
A
A
FR43
FR69
FR43
FR15FWD PAX DOOR
PAX COMPARTMENTEMERGENCY EXIT
PAX COMPARTMENTEMERGENCY EXIT
AFT PAX DOOR
B
C
C
C
C
C
C
C
C
C
- Z230 Z260
B
C
FR66
FR21
CC
C
C
C
C
ICN-A320-A-25XX1BQB-A-FAPE3-00Y3H-A-003-01
A318/A319/A320/A321SERVICE BULLETIN
Figure ICN-A320-A-25XX1BQB-A-FAPE3-00Y3I-A-002-01 SHEET 2/2REV 00 Sep 18/19 A320-25-1BQBInspection of the LH Over-Head Stowage
Compartment X-Fixation Brackets Page 41
CONF 002
ID-LABEL
LIGHTCOVER
BIN ASSEMBLY
ENDOSCOPECAMERA
FILLER PANEL
HOUSING
X-FIXATIONBRACKET
CTYPICAL
VIEW LOOKING FWD
INBD
BIN ASSEMBLY
HOUSING
D
X-FIXATIONBRACKETS
DNOTE:
CAMERA VIEW.01
01
ICN-A320-A-25XX1BQB-A-FAPE3-00Y3I-A-002-01
A318/A319/A320/A321SERVICE BULLETIN
Figure ICN-A320-A-25XX1BQB-A-FAPE3-00YPF-A-009-01 SHEET 1/1REV 00 Sep 18/19 A320-25-1BQBFlowchart
Page 42
CONF 002
YES
NO
E2529400200600, E2529401400600, E2529401600600, E2529401800200, E2529402000600,E2529402200800, E2529402400200, E2529402600600, E2529402800600, E2529404800800,E2529405200600, E2529405600200, E2529405800600, E2529406800200, E2529408800200
DO AN INSPECTION OF LH OHSC LISTED BELOW:
YES
NO
SEND THE COMPLETEDINSPECTION REPORT SHEET
FOUND
IS ANX-FIXATION BRACKET
MISSING?
INSTALLED
IS ANX-FIXATION BRACKET
INCORRECTLY?
INSTALL THE X-FIXATION BRACKET
INSTALL THE X-FIXATION BRACKET
THE PURPOSE OF FLOWCHARTS IS TO SUPPLEMENT THE INFORMATIONGIVEN IN THE PROCEDURE AND COMPLIANCE PARAGRAPHS AND NOT TOSERVE AS THE PRIMARY SOURCE FOR TASKS OR COMPLIANCE TIMESGIVEN IN THIS SERVICE BULLETIN.
NOTE:FOR THE ACCOMPLISHMENT TIMESCALE, REFER TO PARAGRAPH 1.E.(2).01
01
NO FURTHER ACTIONWITH THIS SERVICE
BULLETIN
ICN-A320-A-25XX1BQB-A-FAPE3-00YPF-A-009-01
A318/A319/A320/A321SERVICE BULLETIN
Figure ICN-A320-A-25XX1BQB-A-FAPE3-01IGW-A-001-01 SHEET 1/1REV 00 Sep 18/19 A320-25-1BQBInspection report
Page 43
CONF 002
INSPECTION REPORT
SERVICE BULLETIN No:
A/C MSN :
FLIGHT CYCLES (FC):
FLIGHT HOURS (FH):
A320-25-1BQB
DATE OF INSPECTION:
SEND THE COMPLETED INSPECTION REPORTSHEET IN ACCORDANCE WITH ISI 00.00.00179
INSPECTION METHOD: SPECIAL DETAILEDINSPECTION (SDI)
SDI OF OHSC X-FIXATION BRACKET
PART NUMBER (PN) CHECK OF THE LH OHSC
AFFECTED OHSC PN;
BRACKET NOT INSTALLED:
BRACKET INSTALLED INCORRECTLY:
ICN-A320-A-25XX1BQB-A-FAPE3-01IGW-A-001-01
A318/A319/A320/A321SERVICE BULLETIN
REV 00 Sep 18/19 A320-25-1BQBPage 44
CONF 001(2) Task A320-A-25-XX-1BQB-02001-312A-A - Do an SDI of the X-fixation
Brackets on the RH OHSC using an Endoscope CameraJob Set-Up Information
Working Area
Impacted Zone Access / Work Location230 Work location From Frame 21 to Frame 35240 Work location From Frame 35 to Frame 47250 Work location From Frame 47 to Frame 64260 Work location From Frame 64 to Frame 66
Manpower/Resources/Skills
Man-hours 1.50 hMinimum Number of person 1Elapsed Time 1.50 hSkills Cabin
Referenced Information
Manuals/Drawings References/Sheets
AMM 06-20-00, Page Block 00106-31-53, Page Block 001
ISI 00.00.00179NTM 51-90-00
Procedure(a) Standard Practices
1 For the identification of zones, refer to Ref. AMM 06-20-00, Page Block 001.2 For the Frame (FR) identification, refer to Ref. AMM 06-31-53, Page Block
001.(b) Identify the applicable RH OHSC PNs on the ID label of the OHSC which is located
behind the light cover to do the SDI.Refer to Ref. Fig. Location and Identification of the RH Over-Head StowageCompartment Part Numbers.
(c) Do an SDI of the x-fixation brackets using an endoscope camera insertedbetween the OHSC bin assembly and the filler panel, refer to Ref. NTM 51-90-00.Refer to Ref. Fig. Inspection of the RH Over-Head Stowage Compartment X-Fixation Brackets and Ref. Fig. Flowchart.1 If an x-fixation bracket is found missing, install the bracket in accordance
with:Ref. Task A320-A-25-XX-1BQB-02ZZZ-600Z-AorRef. Task A320-A-25-XX-1BQB-04ZZZ-600Z-AorRef. Task A320-A-25-XX-1BQB-06ZZZ-600Z-AorRef. Task A320-A-25-XX-1BQB-08ZZZ-600Z-A
A318/A319/A320/A321SERVICE BULLETIN
REV 00 Sep 18/19 A320-25-1BQBPage 45
2 If an x-fixation bracket is found installed incorrectly, remove and install thebracket correctly in accordance with:Ref. Task A320-A-25-XX-1BQB-10ZZZ-600Z-AorRef. Task A320-A-25-XX-1BQB-12ZZZ-600Z-AorRef. Task A320-A-25-XX-1BQB-14ZZZ-600Z-AorRef. Task A320-A-25-XX-1BQB-16ZZZ-600Z-A
NOTE: The x-fixation brackets are installed in ‘Flight Direction’ on thefront side of the housing and bin.
NOTE: The x-fixation brackets at OHSC with MCU cover is installed on oneframe, opposite to the ‘Flight Direction’.
3 Complete the Inspection Report Sheet, refer to Ref. Fig. Inspection report.4 Send the completed Inspection Report sheet in accordance with Ref. ISI
00.00.00179.
NOTE: To send the Inspection Report sheet is not Required for Compliance(RC).
5 If the x-fixation brackets are found installed correctly, no further action isnecessary.
A318/A319/A320/A321SERVICE BULLETIN
Figure ICN-A320-A-25XX1BQB-A-FAPE3-01DLV-A-001-01 SHEET 1/3REV 00 Sep 18/19 A320-25-1BQBLocation and Identification of the RH Over-
Head Stowage Compartment Part Numbers Page 46
CONF 001
C
FR43
FR69
FR43
FR15
A 01
NOTE:REFER TO SHEET 03, TABLE 01.01
01B
PAX COMPARTMENTEMERGENCY EXIT
C
C
C
C
C
C
C
C
C
C
B
C
D
E
F
G
H
J
K
L
FWD PAX DOOR
FR21
A
A
B
- Z230 Z260
FR66
AFT PAX DOOR
ICN-A320-A-25XX1BQB-A-FAPE3-01DLV-A-001-01
A318/A319/A320/A321SERVICE BULLETIN
Figure ICN-A320-A-25XX1BQB-A-FAPE3-01DLW-A-001-01 SHEET 2/3REV 00 Sep 18/19 A320-25-1BQBLocation and Identification of the RH Over-
Head Stowage Compartment Part Numbers Page 47
CONF 001
CTYPICAL
VIEW LOOKING FWD
ID-LABEL
LIGHTCOVER
BIN ASSEMBLY
FILLER PANEL
HOUSING
X-FIXATIONBRACKET
INBD
ICN-A320-A-25XX1BQB-A-FAPE3-01DLW-A-001-01
A318/A319/A320/A321SERVICE BULLETIN
Figure ICN-A320-A-25XX1BQB-A-FAPE3-01DLX-A-001-01 SHEET 3/3REV 00 Sep 18/19 A320-25-1BQBLocation and Identification of the RH Over-
Head Stowage Compartment Part Numbers Page 48
CONF 001
1 E2529400100000 4 FR RH OHSC
1 E2529400300800 4 FR RH OHSC
1 E2529400500200 4 FR RH OHSC
1 E2529400700200 4 FR RH OHSC
1 E2529402500000 4 FR RH OHSC
1 E2529401100200 4 FR RH OHSC
1 E2529401300200 4 FR RH OHSC
1 E2529401500400 4 FR RH OHSC
1 E2529401700800 4 FR RH OHSC
1 E2529401900000 4 FR RH OHSC
1 E2529404900800 3 FR RH OHSC
AA
B
C
D
E
F
G
H
J
K
L
POSITION QUANTITY PART NUMBER OHSC VARIANT
TABLE 01
ICN-A320-A-25XX1BQB-A-FAPE3-01DLX-A-001-01
A318/A319/A320/A321SERVICE BULLETIN
Figure ICN-A320-A-25XX1BQB-A-FAPE3-00YPQ-A-003-01 SHEET 1/2REV 00 Sep 18/19 A320-25-1BQBInspection of the RH Over-Head Stowage
Compartment X-Fixation Brackets Page 49
CONF 001
C
FR43
FR69
FR43
FR15
A
B
PAX COMPARTMENTEMERGENCY EXIT
C
C
C
C
C
C
C
C
C
C
FWD PAX DOOR
FR21
A
B
- Z230 Z260
FR66
AFT PAX DOOR
ICN-A320-A-25XX1BQB-A-FAPE3-00YPQ-A-003-01
A318/A319/A320/A321SERVICE BULLETIN
Figure ICN-A320-A-25XX1BQB-A-FAPE3-00YPR-A-002-01 SHEET 2/2REV 00 Sep 18/19 A320-25-1BQBInspection of the RH Over-Head Stowage
Compartment X-Fixation Brackets Page 50
CONF 001
CTYPICAL
VIEW LOOKING FWD
D
ID-LABEL
LIGHTCOVER
BIN ASSEMBLY
ENDOSCOPECAMERA
FILLER PANEL
HOUSING
X-FIXATIONBRACKET
D
INBD
BIN ASSEMBLY
HOUSING
X-FIXATIONBRACKETS
01NOTE:
CAMERA VIEW.01 ICN-A320-A-25XX1BQB-A-FAPE3-00YPR-A-002-01
A318/A319/A320/A321SERVICE BULLETIN
Figure ICN-A320-A-25XX1BQB-A-FAPE3-00Z0T-A-006-01 SHEET 1/1REV 00 Sep 18/19 A320-25-1BQBFlowchart
Page 51
CONF 001
YES
E2529400100000, E2529400300800, E2529400500200, E2529400700200, E2529401100200,E2529401300200, E2529401500400, E2529401700800, E2529401900000, E2529402500000,E2529404900800
DO AN INSPECTION OF RH OHSC LISTED BELOW:
NO
SEND THE COMPLETEDINSPECTION REPORT SHEET
INSTALLED
IS ANX-FIXATION BRACKET
INCORRECTLY?
NOYESFOUND
IS ANX-FIXATION BRACKET
MISSING?
INSTALL THE X-FIXATION BRACKET
INSTALL THE X-FIXATION BRACKET
THE PURPOSE OF FLOWCHARTS IS TO SUPPLEMENT THE INFORMATIONGIVEN IN THE PROCEDURE AND COMPLIANCE PARAGRAPHS AND NOT TOSERVE AS THE PRIMARY SOURCE FOR TASKS OR COMPLIANCE TIMESGIVEN IN THIS SERVICE BULLETIN.
NOTE:FOR THE ACCOMPLISHMENT TIMESCALE, REFER TO PARAGRAPH 1.E.(2).01
01
NO FURTHER ACTIONWITH THIS SERVICE
BULLETIN
ICN-A320-A-25XX1BQB-A-FAPE3-00Z0T-A-006-01
A318/A319/A320/A321SERVICE BULLETIN
Figure ICN-A320-A-25XX1BQB-A-FAPE3-01IHD-A-001-01 SHEET 1/1REV 00 Sep 18/19 A320-25-1BQBInspection report
Page 52
CONF 001
INSPECTION REPORT
SERVICE BULLETIN No:
A/C MSN :
FLIGHT CYCLES (FC):
FLIGHT HOURS (FH):
A320-25-1BQB
DATE OF INSPECTION:
SEND THE COMPLETED INSPECTION REPORTSHEET IN ACCORDANCE WITH ISI 00.00.00179
INSPECTION METHOD: SPECIAL DETAILEDINSPECTION (SDI)
SDI OF OHSC X-FIXATION BRACKET
PART NUMBER (PN) CHECK OF THE RH OHSC
AFFECTED OHSC PN;
BRACKET NOT INSTALLED:
BRACKET INSTALLED INCORRECTLY:
ICN-A320-A-25XX1BQB-A-FAPE3-01IHD-A-001-01
A318/A319/A320/A321SERVICE BULLETIN
REV 00 Sep 18/19 A320-25-1BQBPage 53
CONF 002(2) Task A320-A-25-XX-1BQB-02002-312A-A - Do an SDI of the X-fixation
Brackets on the RH OHSC using an Endoscope CameraJob Set-Up Information
Working Area
Impacted Zone Access / Work Location230 Work location From Frame 21 to Frame 35.8240 Work location From Frame 35.8 to Frame 47250 Work location From Frame 47 to Frame 64260 Work location From Frame 64 to Frame 66
Manpower/Resources/Skills
Man-hours 2.00 hMinimum Number of person 1Elapsed Time 2.00 hSkills Cabin
Referenced Information
Manuals/Drawings References/Sheets
AMM 06-20-00, Page Block 00106-31-53, Page Block 001
ISI 00.00.00179NTM 51-90-00
Procedure(a) Standard Practices
1 For the identification of zones, refer to Ref. AMM 06-20-00, Page Block 001.2 For the Frame (FR) identification, refer to Ref. AMM 06-31-53, Page Block
001.(b) Identify the applicable RH OHSC PNs on the ID label of the OHSC which is located
behind the light cover to do the SDI.Refer to Ref. Fig. Location and Identification of the RH Over-Head StowageCompartment Part Numbers.
(c) Do an SDI of the x-fixation brackets using an endoscope camera insertedbetween the OHSC bin assembly and the filler panel, refer to Ref. NTM 51-90-00.Refer to Ref. Fig. Inspection of the RH Over-Head Stowage Compartment X-Fixation Brackets and Ref. Fig. Flowchart.1 If an x-fixation bracket is found missing, install the bracket in accordance
with:Ref. Task A320-A-25-XX-1BQB-02ZZZ-600Z-AorRef. Task A320-A-25-XX-1BQB-04ZZZ-600Z-A
2 If an x-fixation bracket is found installed incorrectly, remove and install thebracket correctly in accordance with:Ref. Task A320-A-25-XX-1BQB-10ZZZ-600Z-AorRef. Task A320-A-25-XX-1BQB-12ZZZ-600Z-A
A318/A319/A320/A321SERVICE BULLETIN
REV 00 Sep 18/19 A320-25-1BQBPage 54
NOTE: The x-fixation brackets are installed in ‘Flight Direction’ on thefront side of the housing and bin.
NOTE: The x-fixation brackets at OHSC with MCU cover is installed on oneframe, opposite to the ‘Flight Direction’.
3 Complete the Inspection Report Sheet, refer to Ref. Fig. Inspection report.4 Send the completed Inspection Report sheet in accordance with Ref. ISI
00.00.00179.
NOTE: To send the Inspection Report sheet is not Required for Compliance(RC).
5 If the x-fixation brackets are found installed correctly, no further action isnecessary.
A318/A319/A320/A321SERVICE BULLETIN
Figure ICN-A320-A-25XX1BQB-A-FAPE3-01DLP-A-001-01 SHEET 1/3REV 00 Sep 18/19 A320-25-1BQBLocation and Identification of the RH Over-
Head Stowage Compartment Part Numbers Page 55
CONF 002
A
A
B
FR43
FR69
FR43
FR15FWD PAX DOOR
PAX COMPARTMENTEMERGENCY EXIT
PAX COMPARTMENTEMERGENCY EXIT
NOTE:01
NOTE:REFER TO SHEET 03, TABLE 01.01
C
A
B
C
D
EF
G
H
J
K
L
M
N
P
Q
C C
CC
C
C
C
CC
C
C
CC
C
01
01
- Z230 Z260
B
FR21
FR66
AFT PAX DOOR
ICN-A320-A-25XX1BQB-A-FAPE3-01DLP-A-001-01
A318/A319/A320/A321SERVICE BULLETIN
Figure ICN-A320-A-25XX1BQB-A-FAPE3-01DLQ-A-001-01 SHEET 2/3REV 00 Sep 18/19 A320-25-1BQBLocation and Identification of the RH Over-
Head Stowage Compartment Part Numbers Page 56
CONF 002
CTYPICAL
VIEW LOOKING FWD
ID-LABEL
LIGHTCOVER
BIN ASSEMBLY
FILLER PANEL
HOUSING
X-FIXATIONBRACKET
INBD
ICN-A320-A-25XX1BQB-A-FAPE3-01DLQ-A-001-01
A318/A319/A320/A321SERVICE BULLETIN
Figure ICN-A320-A-25XX1BQB-A-FAPE3-01DLR-A-001-01 SHEET 3/3REV 00 Sep 18/19 A320-25-1BQBLocation and Identification of the RH Over-
Head Stowage Compartment Part Numbers Page 57
CONF 002
1 E2529400100400 4 FR RH OHSC
1 E2529400300600 4 FR RH OHSC
1 E2529402100600 4 FR RH OHSC
1 E2529405300600 2 FR RH OHSC
1 E2529405700200 2 FR RH OHSC
1 E2529405900600 2 FR RH OHSC
1 E2529402300800 4 FR RH OHSC
1 E2529402500200 4 FR RH OHSC
1 E2529402700600 4 FR RH OHSC
1 E2529406900200 1 FR RH OHSC
1 E2529402900600 4 FR RH OHSC
1 E2529401500600 4 FR RH OHSC
1 E2529401700600 4 FR RH OHSC
1 E2529401900400 4 FR RH OHSC
1 E2529407100400 1 FR RH OHSC
AA
B
C
D
E
F
G
H
J
K
L
M
N
P
Q
POSITION QUANTITY PART NUMBER OHSC VARIANT
TABLE 01
ICN-A320-A-25XX1BQB-A-FAPE3-01DLR-A-001-01
A318/A319/A320/A321SERVICE BULLETIN
Figure ICN-A320-A-25XX1BQB-A-FAPE3-00YPU-A-003-01 SHEET 1/2REV 00 Sep 18/19 A320-25-1BQBInspection of the RH Over-Head Stowage
Compartment X-Fixation Brackets Page 58
CONF 002
A
A
B
FR43
FR69
FR43
FR15FWD PAX DOOR
PAX COMPARTMENTEMERGENCY EXIT
PAX COMPARTMENTEMERGENCY EXIT
C
C C
CC
C
C
C
CC
C
C
CC
C
- Z230 Z260
B
FR21
FR66
AFT PAX DOOR
ICN-A320-A-25XX1BQB-A-FAPE3-00YPU-A-003-01
A318/A319/A320/A321SERVICE BULLETIN
Figure ICN-A320-A-25XX1BQB-A-FAPE3-00YPV-A-002-01 SHEET 2/2REV 00 Sep 18/19 A320-25-1BQBInspection of the RH Over-Head Stowage
Compartment X-Fixation Brackets Page 59
CONF 002
CTYPICAL
VIEW LOOKING FWD
D
ID-LABEL
LIGHTCOVER
BIN ASSEMBLY
ENDOSCOPECAMERA
FILLER PANEL
HOUSING
X-FIXATIONBRACKET
D
INBD
BIN ASSEMBLY
HOUSING
X-FIXATIONBRACKETS
NOTE:CAMERA VIEW.01
01
ICN-A320-A-25XX1BQB-A-FAPE3-00YPV-A-002-01
A318/A319/A320/A321SERVICE BULLETIN
Figure ICN-A320-A-25XX1BQB-A-FAPE3-00Z0S-A-006-01 SHEET 1/1REV 00 Sep 18/19 A320-25-1BQBFlowchart
Page 60
CONF 002
YES
E2529400100400, E2529400300600, E2529401500600, E2529401700600, E2529401900400,E2529402100600, E2529402300800, E2529402500200, E2529402700600, E2529402900600,E2529405300600, E2529405700200, E2529405900600, E2529406900200, E2529407100400
DO AN INSPECTION OF RH OHSC LISTED BELOW:
NO
SEND THE COMPLETEDINSPECTION REPORT SHEET
INSTALLED
IS ANX-FIXATION BRACKET
INCORRECTLY?
NOYESFOUND
IS ANX-FIXATION BRACKET
MISSING?
INSTALL THE X-FIXATION BRACKET
INSTALL THE X-FIXATION BRACKET
THE PURPOSE OF FLOWCHARTS IS TO SUPPLEMENT THE INFORMATIONGIVEN IN THE PROCEDURE AND COMPLIANCE PARAGRAPHS AND NOT TOSERVE AS THE PRIMARY SOURCE FOR TASKS OR COMPLIANCE TIMESGIVEN IN THIS SERVICE BULLETIN.
NOTE:FOR THE ACCOMPLISHMENT TIMESCALE, REFER TO PARAGRAPH 1.E.(2).01
01
NO FURTHER ACTIONWITH THIS SERVICE
BULLETIN
ICN-A320-A-25XX1BQB-A-FAPE3-00Z0S-A-006-01
A318/A319/A320/A321SERVICE BULLETIN
Figure ICN-A320-A-25XX1BQB-A-FAPE3-01IHD-A-001-01 SHEET 1/1REV 00 Sep 18/19 A320-25-1BQBInspection report
Page 61
CONF 002
INSPECTION REPORT
SERVICE BULLETIN No:
A/C MSN :
FLIGHT CYCLES (FC):
FLIGHT HOURS (FH):
A320-25-1BQB
DATE OF INSPECTION:
SEND THE COMPLETED INSPECTION REPORTSHEET IN ACCORDANCE WITH ISI 00.00.00179
INSPECTION METHOD: SPECIAL DETAILEDINSPECTION (SDI)
SDI OF OHSC X-FIXATION BRACKET
PART NUMBER (PN) CHECK OF THE RH OHSC
AFFECTED OHSC PN;
BRACKET NOT INSTALLED:
BRACKET INSTALLED INCORRECTLY:
ICN-A320-A-25XX1BQB-A-FAPE3-01IHD-A-001-01
A318/A319/A320/A321SERVICE BULLETIN
REV 00 Sep 18/19 A320-25-1BQBPage 62
CONF ALLD. PREPARATION FOR TEST
NoneE. TEST
NoneF. CLOSE-UP
(1) Task A320-A-25-XX-1BQB-01001-740A-A - Close-upJob Set-Up Information
Manpower/Resources/Skills
Man-hours 0.25 hMinimum Number of person 1Elapsed Time 0.25 h
Procedure
NOTE: If you intend to accomplish an associated Repair Task during the same layoverperiod, the subsequent close-up procedure is not necessary.
(a) Make sure that the work areas are clean and clear of tools and other items ofequipment.
(b) Put the aircraft back to its initial configuration.G. ADMINISTRATIVE
(1) Task A320-A-25-XX-1BQB-01001-90AA-A - Administrative
ProcedureConfirm in the applicable aircraft records that you have completed all the work definedin this Service Bulletin task set as required.
A318/A319/A320/A321SERVICE BULLETIN
REV 00 Sep 18/19 A320-25-1BQBPage 63
Task set A320-A-25-XX-1BQB-02000-93BA-AInspection of the X-Fixation Bracket without using Endoscope Camera (Alternative Method)
WARNING: MAKE SURE THAT YOU OBEY ALL THE WARNINGS AND ALL THE CAUTIONSINCLUDED IN THE REFERENCED PROCEDURES.
CAUTION: ALWAYS OBEY THE PRECAUTIONS THAT FOLLOW TO KEEP ELECTRICALWIRING IN A SATISFACTORY CONDITION (ELECTRICALLY AND MECHANICALLYSERVICEABLE). WHEN YOU DO MAINTENANCE WORK, REPAIRS ORMODIFICATIONS, ALWAYS KEEP ELECTRICAL WIRING, COMPONENTS ANDTHE 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 ANDDAMAGE 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 inother 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 thisService 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 stepsto add flexibility to their maintenance operations as long as the technical intent of theService Bulletin is met within the set parameters.
NOTE: Manual titles given in the accomplishment instructions are referred to by acronyms. Referto paragraph 1.J., References, for the definition of acronyms.
NOTE: The purpose of flowcharts is to supplement the information given in the Procedure andCompliance paragraphs and not to serve as the primary source for tasks or compliancetimes given in this Service Bulletin.
NOTE: This Service Bulletin is classified mandatory or expected to be classified mandatory byan Airworthiness Directive (AD). The paragraphs 3.C. and 3.E. in these accomplishmentinstructions 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 theseparagraphs 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 givenin the Service Bulletin, as long as the RC paragraphs can be done and the aircraft can beput back into a serviceable condition.
NOTE: This Service Bulletin contains the instructions for the on-aircraft maintenance necessaryto ensure the continued airworthiness of the aircraft.For any deviations to the instructions, including RC paragraph contained herein, contactAIRBUS for further instructions and approval.
A. TASK SET ASSOCIATED INFORMATIONTask Manpower
CONF 001TOTAL MAN-HOURS 21.50 h
A318/A319/A320/A321SERVICE BULLETIN
REV 00 Sep 18/19 A320-25-1BQBPage 64
CONF 002TOTAL MAN-HOURS 28.50 h
CONF 001ELAPSED TIME (HOURS) 9.50 h
CONF 002ELAPSED TIME (HOURS) 12.50 h
CONF ALLB. PREPARATION
CONF 001(1) Task A320-A-25-XX-1BQB-02001-540A-A - Job Set-up
Job Set-Up InformationManpower/Resources/Skills
Man-hours 9.00 hMinimum Number of person 3Elapsed Time 3.00 h
Referenced Information
Manuals/Drawings References/Sheets
AMM Task 12-34-24-869-002Task 25-24-41-000-802
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 Task12-34-24-869-002.
(b) Do the job-set up procedure as specified in the removal of the bin, refer to Ref.AMM Task 25-24-41-000-802.
CONF 002(1) Task A320-A-25-XX-1BQB-02002-540A-A - Job Set-up
Job Set-Up InformationManpower/Resources/Skills
Man-hours 12.00 hMinimum Number of person 3Elapsed Time 4.00 h
Referenced Information
Manuals/Drawings References/Sheets
AMM Task 12-34-24-869-002Task 25-24-41-000-802
Procedure
NOTE: For the basic Aircraft configuration, refer to AMM Chapter “Introduction -Aircraft status for maintenance" in Manual Front Matter section.
A318/A319/A320/A321SERVICE BULLETIN
REV 00 Sep 18/19 A320-25-1BQBPage 65
(a) Make sure that the aircraft is electrically grounded, refer to Ref. AMM Task12-34-24-869-002.
(b) Do the job-set up procedure as specified in the removal of the bin, refer to Ref.AMM Task 25-24-41-000-802.
CONF ALLC. PROCEDURE
CONF 001(1) Task A320-A-25-XX-1BQB-01001-311A-A - Do an SDI of the X-fixation
Brackets on the LH OHSC without using Endoscope CameraJob Set-Up Information
Working Area
Impacted Zone Access / Work Location230 Work location From Frame 21 to Frame 35240 Work location From Frame 35 to Frame 47250 Work location From Frame 47 to Frame 64260 Work location From Frame 64 to Frame 66
Manpower/Resources/Skills
Man-hours 1.50 hMinimum Number of person 1Elapsed Time 1.50 hSkills Cabin
Referenced Information
Manuals/Drawings References/Sheets
AMM
06-20-00, Page Block 00106-31-53, Page Block 001Task 20-21-11-911-001Task 25-24-41-000-802Task 25-24-41-400-802
ISI 00.00.00179NTM 51-90-00
Procedure(a) Standard Practices
1 For the identification of zones, refer to Ref. AMM 06-20-00, Page Block 001.2 For the Frame (FR) identification, refer to Ref. AMM 06-31-53, Page Block
001.3 Tag all the parts you must remove and retain to make the subsequent
installation easier.4 Put all the retained hardware in identified plastic bags and attach the bags
to the related unit.5 To torque tighten the standard threaded fasteners, refer to Ref. AMM Task
20-21-11-911-001.
A318/A319/A320/A321SERVICE BULLETIN
REV 00 Sep 18/19 A320-25-1BQBPage 66
(b) Identify the applicable LH OHSC PNs on the ID label of the OHSC which is locatedbehind the light cover to do the SDI.Refer to Ref. Fig. Location and Identification of the LH Over-Head StowageCompartment Part Numbers.
(c) Remove the bin from the OHSC, refer to Ref. AMM Task 25-24-41-000-802.(d) Do an SDI of the x-fixation brackets, refer to Ref. NTM 51-90-00 and Ref. Fig.
Flowchart.1 If an x-fixation bracket is found missing, install the bracket in accordance
with:Ref. Task A320-A-25-XX-1BQB-01ZZZ-600Z-AorRef. Task A320-A-25-XX-1BQB-03ZZZ-600Z-AorRef. Task A320-A-25-XX-1BQB-05ZZZ-600Z-AorRef. Task A320-A-25-XX-1BQB-07ZZZ-600Z-A
2 If an x-fixation bracket is found installed incorrectly, remove and install thebracket correctly in accordance with:Ref. Task A320-A-25-XX-1BQB-09ZZZ-600Z-AorRef. Task A320-A-25-XX-1BQB-11ZZZ-600Z-AorRef. Task A320-A-25-XX-1BQB-13ZZZ-600Z-AorRef. Task A320-A-25-XX-1BQB-15ZZZ-600Z-A
NOTE: The x-fixation brackets are installed in ‘Flight Direction’ on thefront side of the housing and bin.
3 Complete the Inspection Report Sheet, refer to Ref. Fig. Inspection report.4 Send the completed Inspection Report sheet in accordance with Ref. ISI
00.00.00179.
NOTE: To send the Inspection Report sheet is not Required for Compliance(RC).
5 If the x-fixation brackets are found installed correctly, no further action isnecessary.
(e) Install the bin in the OHSC, refer to Ref. AMM Task 25-24-41-400-802.
A318/A319/A320/A321SERVICE BULLETIN
Figure ICN-A320-A-25XX1BQB-A-FAPE3-01DLM-A-001-01 SHEET 1/3REV 00 Sep 18/19 A320-25-1BQBLocation and Identification of the LH Over-
Head Stowage Compartment Part Numbers Page 67
CONF 001
FR43
FR69
FR43
FR15
C
C
C
C
C
C
C
C
C
CFWD PAX DOOR
PAX COMPARTMENTEMERGENCY EXIT
AFT PAX DOOR
NOTE:REFER TO SHEET 03, TABLE 01.01
A 01
01B
A
B
C
D
E
F
G
H
J
K
L
FR21
B
- Z230 Z260
FR66
C
A
ICN-A320-A-25XX1BQB-A-FAPE3-01DLM-A-001-01
A318/A319/A320/A321SERVICE BULLETIN
Figure ICN-A320-A-25XX1BQB-A-FAPE3-01DLN-A-001-01 SHEET 2/3REV 00 Sep 18/19 A320-25-1BQBLocation and Identification of the LH Over-
Head Stowage Compartment Part Numbers Page 68
CONF 001
ID-LABEL
LIGHTCOVER
BIN ASSEMBLY
FILLER PANEL
HOUSING
X-FIXATIONBRACKET
CTYPICAL
VIEW LOOKING FWD
INBD
ICN-A320-A-25XX1BQB-A-FAPE3-01DLN-A-001-01
A318/A319/A320/A321SERVICE BULLETIN
Figure ICN-A320-A-25XX1BQB-A-FAPE3-01DLO-A-001-01 SHEET 3/3REV 00 Sep 18/19 A320-25-1BQBLocation and Identification of the LH Over-
Head Stowage Compartment Part Numbers Page 69
CONF 001
A 1 E2529400000000 4 FR LH OHSC
B 1 E2529400200800 4 FR LH OHSC
C 1 E2529400400200 4 FR LH OHSC
D 1 E2529400600200 4 FR LH OHSC
E 1 E2529402400000 4 FR LH OHSC
F 1 E2529401000200 4 FR LH OHSC
G 1 E2529401200200 4 FR LH OHSC
H 1 E2529401400400 4 FR LH OHSC
J 1 E2529401600400 4 FR LH OHSC
K 1 E2529401800000 4 FR LH OHSC
L 1 E2529404801000 3 FR LH OHSC
POSITION QUANTITY PART NUMBER OHSC VARIANT
TABLE 01
ICN-A320-A-25XX1BQB-A-FAPE3-01DLO-A-001-01
A318/A319/A320/A321SERVICE BULLETIN
Figure ICN-A320-A-25XX1BQB-A-FAPE3-00YPG-A-009-01 SHEET 1/1REV 00 Sep 18/19 A320-25-1BQBFlowchart
Page 70
CONF 001
YES
E2529400000000, E2529400200800, E2529400400200, E2529400600200, E2529401000200, E2529401200200, E2529401400400, E2529401600400, E2529401800000, E2529402400000, E2529404801000
DO AN INSPECTION OF LH OHSC LISTED BELOW:
THE PURPOSE OF FLOWCHARTS IS TO SUPPLEMENT THE INFORMATIONGIVEN IN THE PROCEDURE AND COMPLIANCE PARAGRAPHS AND NOT TOSERVE AS THE PRIMARY SOURCE FOR TASKS OR COMPLIANCE TIMESGIVEN IN THIS SERVICE BULLETIN.
NO
SEND THE COMPLETEDINSPECTION REPORT SHEET
INSTALLED
IS ANX-FIXATION BRACKET
INCORRECTLY?
NOYESFOUND
IS ANX-FIXATION BRACKET
MISSING?
INSTALL THE X-FIXATION BRACKET
INSTALL THE X-FIXATION BRACKET
NOTE:FOR THE ACCOMPLISHMENT TIMESCALE, REFER TO PARAGRAPH 1.E.(2).01
01
NO FURTHER ACTIONWITH THIS SERVICE
BULLETIN
ICN-A320-A-25XX1BQB-A-FAPE3-00YPG-A-009-01
A318/A319/A320/A321SERVICE BULLETIN
Figure ICN-A320-A-25XX1BQB-A-FAPE3-01IGW-A-001-01 SHEET 1/1REV 00 Sep 18/19 A320-25-1BQBInspection report
Page 71
CONF 001
INSPECTION REPORT
SERVICE BULLETIN No:
A/C MSN :
FLIGHT CYCLES (FC):
FLIGHT HOURS (FH):
A320-25-1BQB
DATE OF INSPECTION:
SEND THE COMPLETED INSPECTION REPORTSHEET IN ACCORDANCE WITH ISI 00.00.00179
INSPECTION METHOD: SPECIAL DETAILEDINSPECTION (SDI)
SDI OF OHSC X-FIXATION BRACKET
PART NUMBER (PN) CHECK OF THE LH OHSC
AFFECTED OHSC PN;
BRACKET NOT INSTALLED:
BRACKET INSTALLED INCORRECTLY:
ICN-A320-A-25XX1BQB-A-FAPE3-01IGW-A-001-01
A318/A319/A320/A321SERVICE BULLETIN
REV 00 Sep 18/19 A320-25-1BQBPage 72
CONF 002(1) Task A320-A-25-XX-1BQB-01002-311A-A - Do an SDI of the X-fixation
Brackets on the LH OHSC without using Endoscope CameraJob Set-Up Information
Working Area
Impacted Zone Access / Work Location230 Work location From Frame 21 to Frame 35.8240 Work location From Frame 35.8 to Frame 47250 Work location From Frame 47 to Frame 64260 Work location From Frame 64 to Frame 66
Manpower/Resources/Skills
Man-hours 2.00 hMinimum Number of person 1Elapsed Time 2.00 hSkills Cabin
Referenced Information
Manuals/Drawings References/Sheets
AMM
06-20-00, Page Block 00106-31-53, Page Block 001Task 20-21-11-911-001Task 25-24-41-000-802Task 25-24-41-400-802
ISI 00.00.00179NTM 51-90-00
Procedure(a) Standard Practices
1 For the identification of zones, refer to Ref. AMM 06-20-00, Page Block 001.2 For the Frame (FR) identification, refer to Ref. AMM 06-31-53, Page Block
001.3 Tag all the parts you must remove and retain to make the subsequent
installation easier.4 Put all the retained hardware in identified plastic bags and attach the bags
to the related unit.5 To torque tighten the standard threaded fasteners, refer to Ref. AMM Task
20-21-11-911-001.(b) Identify the applicable LH OHSC PNs on the ID label of the OHSC which is located
behind the light cover to do the SDI.Refer to Ref. Fig. Location and Identification of the LH Over-Head StowageCompartment Part Numbers.
(c) Remove the bin from the OHSC, refer to Ref. AMM Task 25-24-41-000-802.(d) Do an SDI of the x-fixation brackets, refer to Ref. NTM 51-90-00 and Ref. Fig.
Flowchart.
A318/A319/A320/A321SERVICE BULLETIN
REV 00 Sep 18/19 A320-25-1BQBPage 73
1 If an x-fixation bracket is found missing, install the bracket in accordancewith:Ref. Task A320-A-25-XX-1BQB-01ZZZ-600Z-AorRef. Task A320-A-25-XX-1BQB-03ZZZ-600Z-AorRef. Task A320-A-25-XX-1BQB-05ZZZ-600Z-AorRef. Task A320-A-25-XX-1BQB-07ZZZ-600Z-A
2 If an x-fixation bracket is found installed incorrectly, remove and install thebracket correctly in accordance with:Ref. Task A320-A-25-XX-1BQB-09ZZZ-600Z-AorRef. Task A320-A-25-XX-1BQB-11ZZZ-600Z-AorRef. Task A320-A-25-XX-1BQB-13ZZZ-600Z-AorRef. Task A320-A-25-XX-1BQB-15ZZZ-600Z-A
NOTE: The x-fixation brackets are installed in ‘Flight Direction’ on thefront side of the housing and bin.
3 Complete the Inspection Report Sheet, refer to Ref. Fig. Inspection report.4 Send the completed Inspection Report sheet in accordance with Ref. ISI
00.00.00179.
NOTE: To send the Inspection Report sheet is not Required for Compliance(RC).
5 If the x-fixation brackets are found installed correctly, no further action isnecessary.
(e) Install the bin in the OHSC, refer to Ref. AMM Task 25-24-41-400-802.
A318/A319/A320/A321SERVICE BULLETIN
Figure ICN-A320-A-25XX1BQB-A-FAPE3-01DLS-A-001-01 SHEET 1/3REV 00 Sep 18/19 A320-25-1BQBLocation and Identification of the LH Over-
Head Stowage Compartment Part Numbers Page 74
CONF 002
A
NOTE:REFER TO SHEET 03, TABLE 01.01
A 01
FR43
FR69
FR43
FR15FWD PAX DOOR
PAX COMPARTMENTEMERGENCY EXIT
PAX COMPARTMENTEMERGENCY EXIT
AFT PAX DOOR
01B
C
C
C
C
C
C
C
C
C
A
B
C
D
EF
G
H
J
KL
M
N
P
Q
- Z230 Z260
B
C
FR66
FR21
CC
C
C
C
C
ICN-A320-A-25XX1BQB-A-FAPE3-01DLS-A-001-01
A318/A319/A320/A321SERVICE BULLETIN
Figure ICN-A320-A-25XX1BQB-A-FAPE3-01DLT-A-001-01 SHEET 2/3REV 00 Sep 18/19 A320-25-1BQBLocation and Identification of the LH Over-
Head Stowage Compartment Part Numbers Page 75
CONF 002
ID-LABEL
LIGHTCOVER
BIN ASSEMBLY
FILLER PANEL
HOUSING
X-FIXATIONBRACKET
CTYPICAL
VIEW LOOKING FWD
INBD
ICN-A320-A-25XX1BQB-A-FAPE3-01DLT-A-001-01
A318/A319/A320/A321SERVICE BULLETIN
Figure ICN-A320-A-25XX1BQB-A-FAPE3-01DLU-A-001-01 SHEET 3/3REV 00 Sep 18/19 A320-25-1BQBLocation and Identification of the LH Over-
Head Stowage Compartment Part Numbers Page 76
CONF 002
A 1 E2529408800200 2 FR LH OHSC
B 1 E2529400200600 4 FR LH OHSC
C 1 E2529402000600 4 FR LH OHSC
D 1 E2529405200600 2 FR LH OHSC
E 1 E2529405600200 2 FR LH OHSC
F 1 E2529405800600 2 FR LH OHSC
G 1 E2529402200800 4 FR LH OHSC
H 1 E2529402400200 4 FR LH OHSC
J 1 E2529402600600 4 FR LH OHSC
K 1 E2529406800200 1 FR LH OHSC
L 1 E2529402800600 4 FR LH OHSC
M 1 E2529401400600 4 FR LH OHSC
N 1 E2529401600600 4 FR LH OHSC
P 1 E2529401800200 4 FR LH OHSC
Q 1 E2529404800800 3 FR LH OHSC
POSITION QUANTITY PART NUMBER OHSC VARIANT
TABLE 01
ICN-A320-A-25XX1BQB-A-FAPE3-01DLU-A-001-01
A318/A319/A320/A321SERVICE BULLETIN
Figure ICN-A320-A-25XX1BQB-A-FAPE3-00YPF-A-009-01 SHEET 1/1REV 00 Sep 18/19 A320-25-1BQBFlowchart
Page 77
CONF 002
YES
NO
E2529400200600, E2529401400600, E2529401600600, E2529401800200, E2529402000600,E2529402200800, E2529402400200, E2529402600600, E2529402800600, E2529404800800,E2529405200600, E2529405600200, E2529405800600, E2529406800200, E2529408800200
DO AN INSPECTION OF LH OHSC LISTED BELOW:
YES
NO
SEND THE COMPLETEDINSPECTION REPORT SHEET
FOUND
IS ANX-FIXATION BRACKET
MISSING?
INSTALLED
IS ANX-FIXATION BRACKET
INCORRECTLY?
INSTALL THE X-FIXATION BRACKET
INSTALL THE X-FIXATION BRACKET
THE PURPOSE OF FLOWCHARTS IS TO SUPPLEMENT THE INFORMATIONGIVEN IN THE PROCEDURE AND COMPLIANCE PARAGRAPHS AND NOT TOSERVE AS THE PRIMARY SOURCE FOR TASKS OR COMPLIANCE TIMESGIVEN IN THIS SERVICE BULLETIN.
NOTE:FOR THE ACCOMPLISHMENT TIMESCALE, REFER TO PARAGRAPH 1.E.(2).01
01
NO FURTHER ACTIONWITH THIS SERVICE
BULLETIN
ICN-A320-A-25XX1BQB-A-FAPE3-00YPF-A-009-01
A318/A319/A320/A321SERVICE BULLETIN
Figure ICN-A320-A-25XX1BQB-A-FAPE3-01IGW-A-001-01 SHEET 1/1REV 00 Sep 18/19 A320-25-1BQBInspection report
Page 78
CONF 002
INSPECTION REPORT
SERVICE BULLETIN No:
A/C MSN :
FLIGHT CYCLES (FC):
FLIGHT HOURS (FH):
A320-25-1BQB
DATE OF INSPECTION:
SEND THE COMPLETED INSPECTION REPORTSHEET IN ACCORDANCE WITH ISI 00.00.00179
INSPECTION METHOD: SPECIAL DETAILEDINSPECTION (SDI)
SDI OF OHSC X-FIXATION BRACKET
PART NUMBER (PN) CHECK OF THE LH OHSC
AFFECTED OHSC PN;
BRACKET NOT INSTALLED:
BRACKET INSTALLED INCORRECTLY:
ICN-A320-A-25XX1BQB-A-FAPE3-01IGW-A-001-01
A318/A319/A320/A321SERVICE BULLETIN
REV 00 Sep 18/19 A320-25-1BQBPage 79
CONF 001(2) Task A320-A-25-XX-1BQB-02001-311A-A - Do an SDI of the X-fixation
Brackets on the RH OHSC without using Endoscope CameraJob Set-Up Information
Working Area
Impacted Zone Access / Work Location230 Work location From Frame 21 to Frame 35240 Work location From Frame 35 to Frame 47250 Work location From Frame 47 to Frame 64260 Work location From Frame 64 to Frame 66
Manpower/Resources/Skills
Man-hours 1.50 hMinimum Number of person 1Elapsed Time 1.50 hSkills Cabin
Referenced Information
Manuals/Drawings References/Sheets
AMM
06-20-00, Page Block 00106-31-53, Page Block 001Task 20-21-11-911-001Task 25-24-41-000-802Task 25-24-41-400-802
ISI 00.00.00179NTM 51-90-00
Procedure(a) Standard Practices
1 For the identification of zones, refer to Ref. AMM 06-20-00, Page Block 001.2 For the Frame (FR) identification, refer to Ref. AMM 06-31-53, Page Block
001.3 Tag all the parts you must remove and retain to make the subsequent
installation easier.4 Put all the retained hardware in identified plastic bags and attach the bags
to the related unit.5 To torque tighten the standard threaded fasteners, refer to Ref. AMM Task
20-21-11-911-001.(b) Identify the applicable RH OHSC PNs on the ID label of the OHSC which is located
behind the light cover to do the SDI.Refer to Ref. Fig. Location and Identification of the RH Over-Head StowageCompartment Part Numbers.
(c) Remove the bin from the OHSC, refer to Ref. AMM Task 25-24-41-000-802.(d) Do an SDI of the x-fixation brackets, refer to Ref. NTM 51-90-00 and Ref. Fig.
Flowchart.
A318/A319/A320/A321SERVICE BULLETIN
REV 00 Sep 18/19 A320-25-1BQBPage 80
1 If an x-fixation bracket is found missing, install the bracket in accordancewith:Ref. Task A320-A-25-XX-1BQB-02ZZZ-600Z-AorRef. Task A320-A-25-XX-1BQB-04ZZZ-600Z-AorRef. Task A320-A-25-XX-1BQB-06ZZZ-600Z-AorRef. Task A320-A-25-XX-1BQB-08ZZZ-600Z-A
2 If an x-fixation bracket is found installed incorrectly, remove and install thebracket correctly in accordance with:Ref. Task A320-A-25-XX-1BQB-10ZZZ-600Z-AorRef. Task A320-A-25-XX-1BQB-12ZZZ-600Z-AorRef. Task A320-A-25-XX-1BQB-14ZZZ-600Z-AorRef. Task A320-A-25-XX-1BQB-16ZZZ-600Z-A
NOTE: The x-fixation brackets are installed in ‘Flight Direction’ on thefront side of the housing and bin.
NOTE: The x-fixation brackets at OHSC with MCU cover is installed on oneframe, opposite to the ‘Flight Direction’.
3 Complete the Inspection Report Sheet, refer to Ref. Fig. Inspection report.4 Send the completed Inspection Report sheet in accordance with Ref. ISI
00.00.00179.
NOTE: To send the Inspection Report sheet is not Required for Compliance(RC).
5 If the x-fixation brackets are found installed correctly, no further action isnecessary.
(e) Install the bin in the OHSC, refer to Ref. AMM Task 25-24-41-400-802.
A318/A319/A320/A321SERVICE BULLETIN
Figure ICN-A320-A-25XX1BQB-A-FAPE3-01DLV-A-001-01 SHEET 1/3REV 00 Sep 18/19 A320-25-1BQBLocation and Identification of the RH Over-
Head Stowage Compartment Part Numbers Page 81
CONF 001
C
FR43
FR69
FR43
FR15
A 01
NOTE:REFER TO SHEET 03, TABLE 01.01
01B
PAX COMPARTMENTEMERGENCY EXIT
C
C
C
C
C
C
C
C
C
C
B
C
D
E
F
G
H
J
K
L
FWD PAX DOOR
FR21
A
A
B
- Z230 Z260
FR66
AFT PAX DOOR
ICN-A320-A-25XX1BQB-A-FAPE3-01DLV-A-001-01
A318/A319/A320/A321SERVICE BULLETIN
Figure ICN-A320-A-25XX1BQB-A-FAPE3-01DLW-A-001-01 SHEET 2/3REV 00 Sep 18/19 A320-25-1BQBLocation and Identification of the RH Over-
Head Stowage Compartment Part Numbers Page 82
CONF 001
CTYPICAL
VIEW LOOKING FWD
ID-LABEL
LIGHTCOVER
BIN ASSEMBLY
FILLER PANEL
HOUSING
X-FIXATIONBRACKET
INBD
ICN-A320-A-25XX1BQB-A-FAPE3-01DLW-A-001-01
A318/A319/A320/A321SERVICE BULLETIN
Figure ICN-A320-A-25XX1BQB-A-FAPE3-01DLX-A-001-01 SHEET 3/3REV 00 Sep 18/19 A320-25-1BQBLocation and Identification of the RH Over-
Head Stowage Compartment Part Numbers Page 83
CONF 001
1 E2529400100000 4 FR RH OHSC
1 E2529400300800 4 FR RH OHSC
1 E2529400500200 4 FR RH OHSC
1 E2529400700200 4 FR RH OHSC
1 E2529402500000 4 FR RH OHSC
1 E2529401100200 4 FR RH OHSC
1 E2529401300200 4 FR RH OHSC
1 E2529401500400 4 FR RH OHSC
1 E2529401700800 4 FR RH OHSC
1 E2529401900000 4 FR RH OHSC
1 E2529404900800 3 FR RH OHSC
AA
B
C
D
E
F
G
H
J
K
L
POSITION QUANTITY PART NUMBER OHSC VARIANT
TABLE 01
ICN-A320-A-25XX1BQB-A-FAPE3-01DLX-A-001-01
A318/A319/A320/A321SERVICE BULLETIN
Figure ICN-A320-A-25XX1BQB-A-FAPE3-00Z0T-A-006-01 SHEET 1/1REV 00 Sep 18/19 A320-25-1BQBFlowchart
Page 84
CONF 001
YES
E2529400100000, E2529400300800, E2529400500200, E2529400700200, E2529401100200,E2529401300200, E2529401500400, E2529401700800, E2529401900000, E2529402500000,E2529404900800
DO AN INSPECTION OF RH OHSC LISTED BELOW:
NO
SEND THE COMPLETEDINSPECTION REPORT SHEET
INSTALLED
IS ANX-FIXATION BRACKET
INCORRECTLY?
NOYESFOUND
IS ANX-FIXATION BRACKET
MISSING?
INSTALL THE X-FIXATION BRACKET
INSTALL THE X-FIXATION BRACKET
THE PURPOSE OF FLOWCHARTS IS TO SUPPLEMENT THE INFORMATIONGIVEN IN THE PROCEDURE AND COMPLIANCE PARAGRAPHS AND NOT TOSERVE AS THE PRIMARY SOURCE FOR TASKS OR COMPLIANCE TIMESGIVEN IN THIS SERVICE BULLETIN.
NOTE:FOR THE ACCOMPLISHMENT TIMESCALE, REFER TO PARAGRAPH 1.E.(2).01
01
NO FURTHER ACTIONWITH THIS SERVICE
BULLETIN
ICN-A320-A-25XX1BQB-A-FAPE3-00Z0T-A-006-01
A318/A319/A320/A321SERVICE BULLETIN
Figure ICN-A320-A-25XX1BQB-A-FAPE3-01IHD-A-001-01 SHEET 1/1REV 00 Sep 18/19 A320-25-1BQBInspection report
Page 85
CONF 001
INSPECTION REPORT
SERVICE BULLETIN No:
A/C MSN :
FLIGHT CYCLES (FC):
FLIGHT HOURS (FH):
A320-25-1BQB
DATE OF INSPECTION:
SEND THE COMPLETED INSPECTION REPORTSHEET IN ACCORDANCE WITH ISI 00.00.00179
INSPECTION METHOD: SPECIAL DETAILEDINSPECTION (SDI)
SDI OF OHSC X-FIXATION BRACKET
PART NUMBER (PN) CHECK OF THE RH OHSC
AFFECTED OHSC PN;
BRACKET NOT INSTALLED:
BRACKET INSTALLED INCORRECTLY:
ICN-A320-A-25XX1BQB-A-FAPE3-01IHD-A-001-01
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REV 00 Sep 18/19 A320-25-1BQBPage 86
CONF 002(2) Task A320-A-25-XX-1BQB-02002-311A-A - Do an SDI of the X-fixation
Brackets on the RH OHSC without using Endoscope CameraJob Set-Up Information
Working Area
Impacted Zone Access / Work Location230 Work location From Frame 21 to Frame 35.8240 Work location From Frame 35.8 to Frame 47250 Work location From Frame 47 to Frame 64260 Work location From Frame 64 to Frame 66
Manpower/Resources/Skills
Man-hours 2.00 hMinimum Number of person 1Elapsed Time 2.00 hSkills Cabin
Referenced Information
Manuals/Drawings References/Sheets
AMM
06-20-00, Page Block 00106-31-53, Page Block 001Task 20-21-11-911-001Task 25-24-41-000-802Task 25-24-41-400-802
ISI 00.00.00179NTM 51-90-00
Procedure(a) Standard Practices
1 For the identification of zones, refer to Ref. AMM 06-20-00, Page Block 001.2 For the Frame (FR) identification, refer to Ref. AMM 06-31-53, Page Block
001.3 Tag all the parts you must remove and retain to make the subsequent
installation easier.4 Put all the retained hardware in identified plastic bags and attach the bags
to the related unit.5 To torque tighten the standard threaded fasteners, refer to Ref. AMM Task
20-21-11-911-001.(b) Identify the applicable RH OHSC PNs on the ID label of the OHSC which is located
behind the light cover to do the SDI.Refer to Ref. Fig. Location and Identification of the RH Over-Head StowageCompartment Part Numbers.
(c) Remove the bin from the OHSC, refer to Ref. AMM Task 25-24-41-000-802.(d) Do an SDI of the x-fixation brackets, refer to Ref. NTM 51-90-00 and Ref. Fig.
Flowchart.
A318/A319/A320/A321SERVICE BULLETIN
REV 00 Sep 18/19 A320-25-1BQBPage 87
1 If an x-fixation bracket is found missing, install the bracket in accordancewith:Ref. Task A320-A-25-XX-1BQB-02ZZZ-600Z-AorRef. Task A320-A-25-XX-1BQB-04ZZZ-600Z-A
2 If an x-fixation bracket is found installed incorrectly, remove and install thebracket correctly in accordance with:Ref. Task A320-A-25-XX-1BQB-10ZZZ-600Z-AorRef. Task A320-A-25-XX-1BQB-12ZZZ-600Z-A
NOTE: The x-fixation brackets are installed in ‘Flight Direction’ on thefront side of the housing and bin.
NOTE: The x-fixation brackets at OHSC with MCU cover is installed on oneframe, opposite to the ‘Flight Direction’.
3 Complete the Inspection Report Sheet, refer to Ref. Fig. Inspection report.4 Send the completed Inspection Report sheet in accordance with Ref. ISI
00.00.00179.
NOTE: To send the Inspection Report sheet is not Required for Compliance(RC).
5 If the x-fixation brackets are found installed correctly, no further action isnecessary.
(e) Install the bin in the OHSC, refer to Ref. AMM Task 25-24-41-400-802.
A318/A319/A320/A321SERVICE BULLETIN
Figure ICN-A320-A-25XX1BQB-A-FAPE3-01DLP-A-001-01 SHEET 1/3REV 00 Sep 18/19 A320-25-1BQBLocation and Identification of the RH Over-
Head Stowage Compartment Part Numbers Page 88
CONF 002
A
A
B
FR43
FR69
FR43
FR15FWD PAX DOOR
PAX COMPARTMENTEMERGENCY EXIT
PAX COMPARTMENTEMERGENCY EXIT
NOTE:01
NOTE:REFER TO SHEET 03, TABLE 01.01
C
A
B
C
D
EF
G
H
J
K
L
M
N
P
Q
C C
CC
C
C
C
CC
C
C
CC
C
01
01
- Z230 Z260
B
FR21
FR66
AFT PAX DOOR
ICN-A320-A-25XX1BQB-A-FAPE3-01DLP-A-001-01
A318/A319/A320/A321SERVICE BULLETIN
Figure ICN-A320-A-25XX1BQB-A-FAPE3-01DLQ-A-001-01 SHEET 2/3REV 00 Sep 18/19 A320-25-1BQBLocation and Identification of the RH Over-
Head Stowage Compartment Part Numbers Page 89
CONF 002
CTYPICAL
VIEW LOOKING FWD
ID-LABEL
LIGHTCOVER
BIN ASSEMBLY
FILLER PANEL
HOUSING
X-FIXATIONBRACKET
INBD
ICN-A320-A-25XX1BQB-A-FAPE3-01DLQ-A-001-01
A318/A319/A320/A321SERVICE BULLETIN
Figure ICN-A320-A-25XX1BQB-A-FAPE3-01DLR-A-001-01 SHEET 3/3REV 00 Sep 18/19 A320-25-1BQBLocation and Identification of the RH Over-
Head Stowage Compartment Part Numbers Page 90
CONF 002
1 E2529400100400 4 FR RH OHSC
1 E2529400300600 4 FR RH OHSC
1 E2529402100600 4 FR RH OHSC
1 E2529405300600 2 FR RH OHSC
1 E2529405700200 2 FR RH OHSC
1 E2529405900600 2 FR RH OHSC
1 E2529402300800 4 FR RH OHSC
1 E2529402500200 4 FR RH OHSC
1 E2529402700600 4 FR RH OHSC
1 E2529406900200 1 FR RH OHSC
1 E2529402900600 4 FR RH OHSC
1 E2529401500600 4 FR RH OHSC
1 E2529401700600 4 FR RH OHSC
1 E2529401900400 4 FR RH OHSC
1 E2529407100400 1 FR RH OHSC
AA
B
C
D
E
F
G
H
J
K
L
M
N
P
Q
POSITION QUANTITY PART NUMBER OHSC VARIANT
TABLE 01
ICN-A320-A-25XX1BQB-A-FAPE3-01DLR-A-001-01
A318/A319/A320/A321SERVICE BULLETIN
Figure ICN-A320-A-25XX1BQB-A-FAPE3-00Z0S-A-006-01 SHEET 1/1REV 00 Sep 18/19 A320-25-1BQBFlowchart
Page 91
CONF 002
YES
E2529400100400, E2529400300600, E2529401500600, E2529401700600, E2529401900400,E2529402100600, E2529402300800, E2529402500200, E2529402700600, E2529402900600,E2529405300600, E2529405700200, E2529405900600, E2529406900200, E2529407100400
DO AN INSPECTION OF RH OHSC LISTED BELOW:
NO
SEND THE COMPLETEDINSPECTION REPORT SHEET
INSTALLED
IS ANX-FIXATION BRACKET
INCORRECTLY?
NOYESFOUND
IS ANX-FIXATION BRACKET
MISSING?
INSTALL THE X-FIXATION BRACKET
INSTALL THE X-FIXATION BRACKET
THE PURPOSE OF FLOWCHARTS IS TO SUPPLEMENT THE INFORMATIONGIVEN IN THE PROCEDURE AND COMPLIANCE PARAGRAPHS AND NOT TOSERVE AS THE PRIMARY SOURCE FOR TASKS OR COMPLIANCE TIMESGIVEN IN THIS SERVICE BULLETIN.
NOTE:FOR THE ACCOMPLISHMENT TIMESCALE, REFER TO PARAGRAPH 1.E.(2).01
01
NO FURTHER ACTIONWITH THIS SERVICE
BULLETIN
ICN-A320-A-25XX1BQB-A-FAPE3-00Z0S-A-006-01
A318/A319/A320/A321SERVICE BULLETIN
Figure ICN-A320-A-25XX1BQB-A-FAPE3-01IHD-A-001-01 SHEET 1/1REV 00 Sep 18/19 A320-25-1BQBInspection report
Page 92
CONF 002
INSPECTION REPORT
SERVICE BULLETIN No:
A/C MSN :
FLIGHT CYCLES (FC):
FLIGHT HOURS (FH):
A320-25-1BQB
DATE OF INSPECTION:
SEND THE COMPLETED INSPECTION REPORTSHEET IN ACCORDANCE WITH ISI 00.00.00179
INSPECTION METHOD: SPECIAL DETAILEDINSPECTION (SDI)
SDI OF OHSC X-FIXATION BRACKET
PART NUMBER (PN) CHECK OF THE RH OHSC
AFFECTED OHSC PN;
BRACKET NOT INSTALLED:
BRACKET INSTALLED INCORRECTLY:
ICN-A320-A-25XX1BQB-A-FAPE3-01IHD-A-001-01
A318/A319/A320/A321SERVICE BULLETIN
REV 00 Sep 18/19 A320-25-1BQBPage 93
CONF ALLD. PREPARATION FOR TEST
NoneE. TEST
CONF 001(1) Task A320-A-25-XX-1BQB-02001-340A-A - Testing
Job Set-Up InformationWorking Area
Impacted Zone Access / Work Location230 Work location From Frame 21 to Frame 35240 Work location From Frame 35 to Frame 47250 Work location From Frame 47 to Frame 64260 Work location From Frame 64 to Frame 66
Manpower/Resources/Skills
Man-hours 0.50 hMinimum Number of person 1Elapsed Time 0.50 hSkills Cabin
Referenced Information
Manuals/Drawings References/SheetsAMM Task 25-24-00-710-002
Procedure(a) If necessary, do the adjustment of the OHSC bin assembly, refer to Ref. AMM
Task 25-24-00-710-002.CONF 002
(1) Task A320-A-25-XX-1BQB-02002-340A-A - TestingJob Set-Up Information
Working Area
Impacted Zone Access / Work Location230 Work location From Frame 21 to Frame 35.8240 Work location From Frame 35.8 to Frame 47250 Work location From Frame 47 to Frame 64260 Work location From Frame 64 to Frame 66
Manpower/Resources/Skills
Man-hours 0.50 hMinimum Number of person 1Elapsed Time 0.50 hSkills Cabin
A318/A319/A320/A321SERVICE BULLETIN
REV 00 Sep 18/19 A320-25-1BQBPage 94
Referenced Information
Manuals/Drawings References/SheetsAMM Task 25-24-00-710-002
Procedure(a) If necessary, do the adjustment of the OHSC bin assembly, refer to Ref. AMM
Task 25-24-00-710-002.CONF ALL
F. CLOSE-UPCONF 001
(1) Task A320-A-25-XX-1BQB-02001-740A-A - Close-upJob Set-Up Information
Manpower/Resources/Skills
Man-hours 9.00 hMinimum Number of person 3Elapsed Time 3.00 h
Referenced Information
Manuals/Drawings References/SheetsAMM Task 25-24-41-400-802
Procedure
NOTE: If you intend to accomplish an associated Repair Task during the same layoverperiod, the subsequent close-up procedure is not necessary.
(a) Make sure that the work areas are clean and clear of tools and other items ofequipment.
(b) Do the close-up procedure as specified in the installation of the bin, refer to Ref.AMM Task 25-24-41-400-802.
(c) Put the aircraft back to its initial configuration.CONF 002
(1) Task A320-A-25-XX-1BQB-02002-740A-A - Close-upJob Set-Up Information
Manpower/Resources/Skills
Man-hours 12.00 hMinimum Number of person 3Elapsed Time 4.00 h
Referenced Information
Manuals/Drawings References/SheetsAMM Task 25-24-41-400-802
Procedure
NOTE: If you intend to accomplish an associated Repair Task during the same layoverperiod, the subsequent close-up procedure is not necessary.
A318/A319/A320/A321SERVICE BULLETIN
REV 00 Sep 18/19 A320-25-1BQBPage 95
(a) Make sure that the work areas are clean and clear of tools and other items ofequipment.
(b) Do the close-up procedure as specified in the installation of the bin, refer to Ref.AMM Task 25-24-41-400-802.
(c) Put the aircraft back to its initial configuration.CONF ALL
G. ADMINISTRATIVE(1) Task A320-A-25-XX-1BQB-02001-90AA-A - Administrative
ProcedureConfirm in the applicable aircraft records that you have completed all the work definedin this Service Bulletin task set as required.
A318/A319/A320/A321SERVICE BULLETIN
REV 00 Sep 18/19 A320-25-1BQBPage 96
Task set A320-A-25-XX-1BQB-01000-93CA-ARepair (Depending on the Inspection Result)
WARNING: MAKE SURE THAT YOU OBEY ALL THE WARNINGS AND ALL THE CAUTIONSINCLUDED IN THE REFERENCED PROCEDURES.
CAUTION: ALWAYS OBEY THE PRECAUTIONS THAT FOLLOW TO KEEP ELECTRICALWIRING IN A SATISFACTORY CONDITION (ELECTRICALLY AND MECHANICALLYSERVICEABLE). WHEN YOU DO MAINTENANCE WORK, REPAIRS ORMODIFICATIONS, ALWAYS KEEP ELECTRICAL WIRING, COMPONENTS ANDTHE 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 ANDDAMAGE 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 inother 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 thisService 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 stepsto add flexibility to their maintenance operations as long as the technical intent of theService Bulletin is met within the set parameters.
NOTE: Manual titles given in the accomplishment instructions are referred to by acronyms. Referto paragraph 1.J., References, for the definition of acronyms.
NOTE: This Service Bulletin is classified mandatory or expected to be classified mandatory byan Airworthiness Directive (AD). The paragraphs 3.C. and 3.E. in these accomplishmentinstructions 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 theseparagraphs 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 givenin the Service Bulletin, as long as the RC paragraphs can be done and the aircraft can beput back into a serviceable condition.
NOTE: This Service Bulletin contains the instructions for the on-aircraft maintenance necessaryto ensure the continued airworthiness of the aircraft.For any deviations to the instructions, including RC paragraph contained herein, contactAIRBUS for further instructions and approval.
A. TASK SET ASSOCIATED INFORMATIONTask Manpower
CONF 001TOTAL MAN-HOURS 22.50 h
CONF 002TOTAL MAN-HOURS 27.50 h
CONF 001ELAPSED TIME (HOURS) 10.50 h
A318/A319/A320/A321SERVICE BULLETIN
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CONF 002ELAPSED TIME (HOURS) 11.50 h
CONF ALLB. PREPARATION
CONF 001(1) Task A320-A-25-XX-1BQB-03001-540A-A - Job Set-up
Job Set-Up InformationManpower/Resources/Skills
Man-hours 9.00 hMinimum Number of person 3Elapsed Time 3.00 h
Referenced Information
Manuals/Drawings References/Sheets
AMM Task 12-34-24-869-002Task 25-24-41-000-802
Procedure
NOTE: If you intend to accomplish this Repair during the same layover period as theAlternative Method Inspection, the subsequent Preparation procedure is notnecessary.
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 Task12-34-24-869-002.
(b) Do the job-set up procedure as specified in the removal of the bin, refer to Ref.AMM Task 25-24-41-000-802.
CONF 002(1) Task A320-A-25-XX-1BQB-03002-540A-A - Job Set-up
Job Set-Up InformationManpower/Resources/Skills
Man-hours 12.00 hMinimum Number of person 3Elapsed Time 4.00 h
Referenced Information
Manuals/Drawings References/Sheets
AMM Task 12-34-24-869-002Task 25-24-41-000-802
Procedure
NOTE: If you intend to accomplish this Repair during the same layover period as theAlternative Method Inspection, the subsequent Preparation procedure is notnecessary.
A318/A319/A320/A321SERVICE BULLETIN
REV 00 Sep 18/19 A320-25-1BQBPage 98
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 Task12-34-24-869-002.
(b) Do the job-set up procedure as specified in the removal of the bin, refer to Ref.AMM Task 25-24-41-000-802.
CONF ALLC. PROCEDURE
CONF 001(1) Task A320-A-25-XX-1BQB-01001-600A-A - Install the Missing X-Fixation
Bracket on the LH OHSC Bin AssemblyJob Set-Up Information
Working Area
Impacted Zone Access / Work Location230 Work location From Frame 21 to Frame 35240 Work location From Frame 35 to Frame 47250 Work location From Frame 47 to Frame 63
Manpower/Resources/Skills
Man-hours 0.25 hMinimum Number of person 1Elapsed Time 0.25 hSkills Cabin
Material necessary to do the jobComponentsITEM PART No. QTY (UM) KEYWORD DRAWING SEE NOTES1 606A00305-000 1 BRACKET (1)6 NAS1801-08-5 4 SCREW (1)7 NAS1149CN832R 4 WASHER (1)NOTE(S)(1): The components listed above are not an AIRBUS Kit, the required parts must be
ordered as necessary through the given channel.
Referenced Information
Manuals/Drawings References/Sheets
AMM06-20-00, Page Block 00106-31-53, Page Block 001Task 20-21-11-911-001Task 25-24-41-000-802
Procedure(a) Standard Practices
1 For the identification of zones, refer to Ref. AMM 06-20-00, Page Block 001.2 For the Frame (FR) identification, refer to Ref. AMM 06-31-53, Page Block
001.
A318/A319/A320/A321SERVICE BULLETIN
REV 00 Sep 18/19 A320-25-1BQBPage 99
3 Tag all the parts you must remove and retain to make the subsequentinstallation easier.
4 Put all the retained hardware in identified plastic bags and attach the bagsto the related unit.
5 To torque tighten the standard threaded fasteners, refer to Ref. AMM Task20-21-11-911-001.
(b) Install the missing x-fixation bracket on the LH OHSC bin assembly.Refer to Ref. Fig. Installation of the Missing X-Fixation Bracket on the LH Over-Head Stowage Compartment Bin Assembly1 Remove the bin from the LH OHSC, refer to Ref. AMM Task
25-24-41-000-802.2 Install:
Refer to Ref. Fig. Installation of the Missing X-Fixation Bracket on the LHOver-Head Stowage Compartment Bin Assembly
1 BRACKET 606A00305-000 Item 1with
4 SCREW NAS1801-08-5 Item 6
4 WASHER NAS1149CN832R Item 73 Make sure that the bracket item 1 is installed in ‘Flight Direction’ on the
bin assembly, aft of the bracket of the housing, to face each other, refer toRef. Fig. Installation of the Missing X-Fixation Bracket on the LH Over-HeadStowage Compartment Bin Assembly.
4 Torque the screws item 6 to 2.50 Nm (22.126 lbf.in.).
A318/A319/A320/A321SERVICE BULLETIN
Figure ICN-A320-A-25XX1BQB-A-FAPE3-00Y3L-A-003-01 SHEET 1/2REV 00 Sep 18/19 A320-25-1BQBInstallation of the Missing X-Fixation Bracket on the
LH Over-Head Stowage Compartment Bin Assembly Page 100
CONF 001
- Z230 Z250
A
ATYPICAL
VIEW LOOKING AFT
TYPICALVIEW SHOWN WITHOUT HOUSING
B
A
A
BIN
C
B
ICN-A320-A-25XX1BQB-A-FAPE3-00Y3L-A-003-01
A318/A319/A320/A321SERVICE BULLETIN
Figure ICN-A320-A-25XX1BQB-A-FAPE3-01DM1-A-001-01 SHEET 2/2REV 00 Sep 18/19 A320-25-1BQBInstallation of the Missing X-Fixation Bracket on the
LH Over-Head Stowage Compartment Bin Assembly Page 101
CONF 001
67
1
C
AAFWD
VIEW LOOKING DOWN
CLEARANCE2 mm
(0.079 in)
X-FIXATION BRACKETX-FIXATION BRACKET
HOUSING
BIN
BIN
ICN-A320-A-25XX1BQB-A-FAPE3-01DM1-A-001-01
A318/A319/A320/A321SERVICE BULLETIN
REV 00 Sep 18/19 A320-25-1BQBPage 102
CONF 002(1) Task A320-A-25-XX-1BQB-01002-600A-A - Install the Missing X-Fixation
Bracket on the LH OHSC Bin AssemblyJob Set-Up Information
Working Area
Impacted Zone Access / Work Location230 Work location From Frame 21 to Frame 35.8240 Work location From Frame 35.8 to Frame 47250 Work location From Frame 47 to Frame 63
Manpower/Resources/Skills
Man-hours 0.25 hMinimum Number of person 1Elapsed Time 0.25 hSkills Cabin
Material necessary to do the jobComponentsITEM PART No. QTY (UM) KEYWORD DRAWING SEE NOTES1 606A00305-000 1 BRACKET (1)6 NAS1801-08-5 4 SCREW (1)7 NAS1149CN832R 4 WASHER (1)NOTE(S)(1): The components listed above are not an AIRBUS Kit, the required parts must be
ordered as necessary through the given channel.
Referenced Information
Manuals/Drawings References/Sheets
AMM06-20-00, Page Block 00106-31-53, Page Block 001Task 20-21-11-911-001Task 25-24-41-000-802
Procedure(a) Standard Practices
1 For the identification of zones, refer to Ref. AMM 06-20-00, Page Block 001.2 For the Frame (FR) identification, refer to Ref. AMM 06-31-53, Page Block
001.3 Tag all the parts you must remove and retain to make the subsequent
installation easier.4 Put all the retained hardware in identified plastic bags and attach the bags
to the related unit.5 To torque tighten the standard threaded fasteners, refer to Ref. AMM Task
20-21-11-911-001.(b) Install the missing x-fixation bracket on the LH OHSC bin assembly.
Refer to Ref. Fig. Installation of the Missing X-Fixation Bracket on the LH Over-Head Stowage Compartment Bin Assembly
A318/A319/A320/A321SERVICE BULLETIN
REV 00 Sep 18/19 A320-25-1BQBPage 103
1 Remove the bin from the LH OHSC, refer to Ref. AMM Task25-24-41-000-802.
2 Install:Refer to Ref. Fig. Installation of the Missing X-Fixation Bracket on the LHOver-Head Stowage Compartment Bin Assembly
1 BRACKET 606A00305-000 Item 1with
4 SCREW NAS1801-08-5 Item 6
4 WASHER NAS1149CN832R Item 73 Make sure that the bracket item 1 is installed in ‘Flight Direction’ on the
bin assembly, aft of the bracket of the housing, to face each other, refer toRef. Fig. Installation of the Missing X-Fixation Bracket on the LH Over-HeadStowage Compartment Bin Assembly.
4 Torque the screws item 6 to 2.50 Nm (22.126 lbf.in.).
A318/A319/A320/A321SERVICE BULLETIN
Figure ICN-A320-A-25XX1BQB-A-FAPE3-01DLY-A-001-01 SHEET 1/2REV 00 Sep 18/19 A320-25-1BQBInstallation of the Missing X-Fixation Bracket on the
LH Over-Head Stowage Compartment Bin Assembly Page 104
CONF 002
ATYPICAL
VIEW LOOKING AFT
TYPICALVIEW SHOWN WITHOUT HOUSING
B
A
A
BIN
C
B
A
- Z230 Z250
ICN-A320-A-25XX1BQB-A-FAPE3-01DLY-A-001-01
A318/A319/A320/A321SERVICE BULLETIN
Figure ICN-A320-A-25XX1BQB-A-FAPE3-01DLZ-A-001-01 SHEET 2/2REV 00 Sep 18/19 A320-25-1BQBInstallation of the Missing X-Fixation Bracket on the
LH Over-Head Stowage Compartment Bin Assembly Page 105
CONF 002
67
1
C
AAFWD
VIEW LOOKING DOWN
CLEARANCE2 mm
(0.079 in)
X-FIXATION BRACKETX-FIXATION BRACKET
HOUSING
BIN
BIN
ICN-A320-A-25XX1BQB-A-FAPE3-01DLZ-A-001-01
A318/A319/A320/A321SERVICE BULLETIN
REV 00 Sep 18/19 A320-25-1BQBPage 106
CONF 001(2) Task A320-A-25-XX-1BQB-02001-600A-A - Install the Missing X-Fixation
Bracket on the RH OHSC Bin AssemblyJob Set-Up Information
Working Area
Impacted Zone Access / Work Location230 Work location From Frame 21 to Frame 35240 Work location From Frame 35 to Frame 47250 Work location From Frame 47 to Frame 63
Manpower/Resources/Skills
Man-hours 0.25 hMinimum Number of person 1Elapsed Time 0.25 hSkills Cabin
Material necessary to do the jobComponentsITEM PART No. QTY (UM) KEYWORD DRAWING SEE NOTES2 606A00305-001 1 BRACKET (1)6 NAS1801-08-5 4 SCREW (1)7 NAS1149CN832R 4 WASHER (1)NOTE(S)(1): The components listed above are not an AIRBUS Kit, the required parts must be
ordered as necessary through the given channel.
Referenced Information
Manuals/Drawings References/Sheets
AMM06-20-00, Page Block 00106-31-53, Page Block 001Task 20-21-11-911-001Task 25-24-41-000-802
Procedure(a) Standard Practices
1 For the identification of zones, refer to Ref. AMM 06-20-00, Page Block 001.2 For the Frame (FR) identification, refer to Ref. AMM 06-31-53, Page Block
001.3 Tag all the parts you must remove and retain to make the subsequent
installation easier.4 Put all the retained hardware in identified plastic bags and attach the bags
to the related unit.5 To torque tighten the standard threaded fasteners, refer to Ref. AMM Task
20-21-11-911-001.(b) Install the missing x-fixation bracket on the RH OHSC bin assembly.
Refer to Ref. Fig. Installation of the Missing X-Fixation Bracket on the RH Over-Head Stowage Compartment Bin Assembly
A318/A319/A320/A321SERVICE BULLETIN
REV 00 Sep 18/19 A320-25-1BQBPage 107
1 Remove the bin from the RH OHSC, refer to Ref. AMM Task25-24-41-000-802.
2 Install:Refer to Ref. Fig. Installation of the Missing X-Fixation Bracket on the RHOver-Head Stowage Compartment Bin Assembly
1 BRACKET 606A00305-001 Item 2with
4 SCREW NAS1801-08-5 Item 6
4 WASHER NAS1149CN832R Item 73 Make sure that the bracket item 2 is installed in ‘Flight Direction’ on the
bin assembly, aft of the bracket of the housing, to face each other, refer toRef. Fig. Installation of the Missing X-Fixation Bracket on the RH Over-HeadStowage Compartment Bin Assembly.
4 Torque the screws item 6 to 2.50 Nm (22.126 lbf.in.).
A318/A319/A320/A321SERVICE BULLETIN
Figure ICN-A320-A-25XX1BQB-A-FAPE3-00Y3E-A-003-01 SHEET 1/2REV 00 Sep 18/19 A320-25-1BQBInstallation of the Missing X-Fixation Bracket on the
RH Over-Head Stowage Compartment Bin Assembly Page 108
CONF 001
- Z230 Z250
A
ATYPICAL
VIEW LOOKING AFT
TYPICALVIEW SHOWN WITHOUT HOUSING
B
A
A
BIN
C
B
ICN-A320-A-25XX1BQB-A-FAPE3-00Y3E-A-003-01
A318/A319/A320/A321SERVICE BULLETIN
Figure ICN-A320-A-25XX1BQB-A-FAPE3-01DM0-A-001-01 SHEET 2/2REV 00 Sep 18/19 A320-25-1BQBInstallation of the Missing X-Fixation Bracket on the
RH Over-Head Stowage Compartment Bin Assembly Page 109
CONF 001
C
AAVIEW LOOKING DOWN
6
7
2
BIN
CLEARANCE2 mm
(0.079 in)
X-FIXATION BRACKETX-FIXATION BRACKET
HOUSING
BIN
FWD
ICN-A320-A-25XX1BQB-A-FAPE3-01DM0-A-001-01
A318/A319/A320/A321SERVICE BULLETIN
REV 00 Sep 18/19 A320-25-1BQBPage 110
CONF 002(2) Task A320-A-25-XX-1BQB-02002-600A-A - Install the Missing X-Fixation
Bracket on the RH OHSC Bin AssemblyJob Set-Up Information
Working Area
Impacted Zone Access / Work Location230 Work location From Frame 21 to Frame 35.8240 Work location From Frame 35.8 to Frame 47250 Work location From Frame 47 to Frame 64260 Work location From Frame 64 to Frame 66
Manpower/Resources/Skills
Man-hours 0.25 hMinimum Number of person 1Elapsed Time 0.25 hSkills Cabin
Material necessary to do the jobComponentsITEM PART No. QTY (UM) KEYWORD DRAWING SEE NOTES2 606A00305-001 1 BRACKET (1)6 NAS1801-08-5 4 SCREW (1)7 NAS1149CN832R 4 WASHER (1)NOTE(S)(1): The components listed above are not an AIRBUS Kit, the required parts must be
ordered as necessary through the given channel.
Referenced Information
Manuals/Drawings References/Sheets
AMM06-20-00, Page Block 00106-31-53, Page Block 001Task 20-21-11-911-001Task 25-24-41-000-802
Procedure(a) Standard Practices
1 For the identification of zones, refer to Ref. AMM 06-20-00, Page Block 001.2 For the Frame (FR) identification, refer to Ref. AMM 06-31-53, Page Block
001.3 Tag all the parts you must remove and retain to make the subsequent
installation easier.4 Put all the retained hardware in identified plastic bags and attach the bags
to the related unit.5 To torque tighten the standard threaded fasteners, refer to Ref. AMM Task
20-21-11-911-001.
A318/A319/A320/A321SERVICE BULLETIN
REV 00 Sep 18/19 A320-25-1BQBPage 111
(b) Install the missing x-fixation bracket on the RH OHSC bin assembly.Refer to Ref. Fig. Installation of the Missing X-Fixation Bracket on the RH Over-Head Stowage Compartment Bin Assembly1 Remove the bin from the RH OHSC, refer to Ref. AMM Task
25-24-41-000-802.2 Install:
Refer to Ref. Fig. Installation of the Missing X-Fixation Bracket on the RHOver-Head Stowage Compartment Bin Assembly
1 BRACKET 606A00305-001 Item 2with
4 SCREW NAS1801-08-5 Item 6
4 WASHER NAS1149CN832R Item 73 Make sure that the bracket item 2 is installed in ‘Flight Direction’ on the
bin assembly, aft of the bracket of the housing, to face each other, refer toRef. Fig. Installation of the Missing X-Fixation Bracket on the RH Over-HeadStowage Compartment Bin Assembly.
4 Torque the screws item 6 to 2.50 Nm (22.126 lbf.in.).
A318/A319/A320/A321SERVICE BULLETIN
Figure ICN-A320-A-25XX1BQB-A-FAPE3-01DM9-A-002-01 SHEET 1/2REV 00 Sep 18/19 A320-25-1BQBInstallation of the Missing X-Fixation Bracket on the
RH Over-Head Stowage Compartment Bin Assembly Page 112
CONF 002
ATYPICAL
VIEW LOOKING AFT
TYPICALVIEW SHOWN WITHOUT HOUSING
B
BIN
C
B
A
- Z230 Z260
A
A
ICN-A320-A-25XX1BQB-A-FAPE3-01DM9-A-002-01
A318/A319/A320/A321SERVICE BULLETIN
Figure ICN-A320-A-25XX1BQB-A-FAPE3-01DMA-A-001-01 SHEET 2/2REV 00 Sep 18/19 A320-25-1BQBInstallation of the Missing X-Fixation Bracket on the
RH Over-Head Stowage Compartment Bin Assembly Page 113
CONF 002
C
AAVIEW LOOKING DOWN
6
7
2
CLEARANCE2 mm
(0.079 in)
X-FIXATION BRACKETX-FIXATION BRACKET
HOUSING
BIN
FWD
BIN
ICN-A320-A-25XX1BQB-A-FAPE3-01DMA-A-001-01
A318/A319/A320/A321SERVICE BULLETIN
REV 00 Sep 18/19 A320-25-1BQBPage 114
CONF 001(3) Task A320-A-25-XX-1BQB-03001-600A-A - Install the Missing X-Fixation
Bracket on the LH OHSC Housing AssemblyJob Set-Up Information
Working Area
Impacted Zone Access / Work Location230 Work location From Frame 21 to Frame 35240 Work location From Frame 35 to Frame 47250 Work location From Frame 47 to Frame 63
Manpower/Resources/Skills
Man-hours 0.25 hMinimum Number of person 1Elapsed Time 0.25 hSkills Cabin
Material necessary to do the jobComponentsITEM PART No. QTY (UM) KEYWORD DRAWING SEE NOTES1 606A00305-000 1 BRACKET (1)6 NAS1801-08-5 4 SCREW (1)7 NAS1149CN832R 4 WASHER (1)NOTE(S)(1): The components listed above are not an AIRBUS Kit, the required parts must be
ordered as necessary through the given channel.
Referenced Information
Manuals/Drawings References/Sheets
AMM06-20-00, Page Block 00106-31-53, Page Block 001Task 20-21-11-911-001Task 25-24-41-400-802
Procedure(a) Standard Practices
1 For the identification of zones, refer to Ref. AMM 06-20-00, Page Block 001.2 For the Frame (FR) identification, refer to Ref. AMM 06-31-53, Page Block
001.3 Tag all the parts you must remove and retain to make the subsequent
installation easier.4 Put all the retained hardware in identified plastic bags and attach the bags
to the related unit.5 To torque tighten the standard threaded fasteners, refer to Ref. AMM Task
20-21-11-911-001.(b) Install the missing x-fixation bracket on the LH OHSC housing.
Refer to Ref. Fig. Installation of the Missing X-Fixation Bracket on the LH Over-Head Stowage Compartment Housing Assembly
A318/A319/A320/A321SERVICE BULLETIN
REV 00 Sep 18/19 A320-25-1BQBPage 115
1 Install:Refer to Ref. Fig. Installation of the Missing X-Fixation Bracket on the LHOver-Head Stowage Compartment Housing Assembly
1 BRACKET 606A00305-000 Item 1with
4 SCREW NAS1801-08-5 Item 6
4 WASHER NAS1149CN832R Item 72 Make sure that the bracket item 1 is installed in ‘Flight Direction’ on the
housing, in front of the bracket of the bin assembly, to face each other,refer to Ref. Fig. Installation of the Missing X-Fixation Bracket on the LHOver-Head Stowage Compartment Housing Assembly.
3 Torque the screws item 6 to 2.50 Nm (22.126 lbf.in.).4 Install the bin on the LH OHSC, refer to Ref. AMM Task 25-24-41-400-802.
A318/A319/A320/A321SERVICE BULLETIN
Figure ICN-A320-A-25XX1BQB-A-FAPE3-00Y3K-A-003-01 SHEET 1/2REV 00 Sep 18/19 A320-25-1BQBInstallation of the Missing X-Fixation Bracket on the LH
Over-Head Stowage Compartment Housing Assembly Page 116
CONF 001
B
VIEW SHOWN WITHOUT BINSTYPICAL
- Z230 Z250
A
ATYPICAL
VIEW LOOKING AFT
C
HOUSING
C
A
A
A
A
B
ICN-A320-A-25XX1BQB-A-FAPE3-00Y3K-A-003-01
A318/A319/A320/A321SERVICE BULLETIN
Figure ICN-A320-A-25XX1BQB-A-FAPE3-01DMG-A-001-01 SHEET 2/2REV 00 Sep 18/19 A320-25-1BQBInstallation of the Missing X-Fixation Bracket on the LH
Over-Head Stowage Compartment Housing Assembly Page 117
CONF 001
TYPICAL
HOUSING
VIEW LOOKING DOWN
AA FWD
CLEARANCE2 mm
(0.079 in)
X-FIXATION BRACKETX-FIXATION BRACKET
BIN
HOUSING
67
1
C
ICN-A320-A-25XX1BQB-A-FAPE3-01DMG-A-001-01
A318/A319/A320/A321SERVICE BULLETIN
REV 00 Sep 18/19 A320-25-1BQBPage 118
CONF 002(3) Task A320-A-25-XX-1BQB-03002-600A-A - Install the Missing X-Fixation
Bracket on the LH OHSC Housing AssemblyJob Set-Up Information
Working Area
Impacted Zone Access / Work Location230 Work location From Frame 21 to Frame 35.8240 Work location From Frame 35.8 to Frame 47250 Work location From Frame 47 to Frame 63
Manpower/Resources/Skills
Man-hours 0.25 hMinimum Number of person 1Elapsed Time 0.25 hSkills Cabin
Material necessary to do the jobComponentsITEM PART No. QTY (UM) KEYWORD DRAWING SEE NOTES1 606A00305-000 1 BRACKET (1)6 NAS1801-08-5 4 SCREW (1)7 NAS1149CN832R 4 WASHER (1)NOTE(S)(1): The components listed above are not an AIRBUS Kit, the required parts must be
ordered as necessary through the given channel.
Referenced Information
Manuals/Drawings References/Sheets
AMM06-20-00, Page Block 00106-31-53, Page Block 001Task 20-21-11-911-001Task 25-24-41-400-802
Procedure(a) Standard Practices
1 For the identification of zones, refer to Ref. AMM 06-20-00, Page Block 001.2 For the Frame (FR) identification, refer to Ref. AMM 06-31-53, Page Block
001.3 Tag all the parts you must remove and retain to make the subsequent
installation easier.4 Put all the retained hardware in identified plastic bags and attach the bags
to the related unit.5 To torque tighten the standard threaded fasteners, refer to Ref. AMM Task
20-21-11-911-001.(b) Install the missing x-fixation bracket on the LH OHSC housing.
Refer to Ref. Fig. Installation of the Missing X-Fixation Bracket on the LH Over-Head Stowage Compartment Housing Assembly
A318/A319/A320/A321SERVICE BULLETIN
REV 00 Sep 18/19 A320-25-1BQBPage 119
1 Install:Refer to Ref. Fig. Installation of the Missing X-Fixation Bracket on the LHOver-Head Stowage Compartment Housing Assembly
1 BRACKET 606A00305-000 Item 1with
4 SCREW NAS1801-08-5 Item 6
4 WASHER NAS1149CN832R Item 72 Make sure that the bracket item 1 is installed in ‘Flight Direction’ on the
housing, in front of the bracket of the bin assembly, to face each other,refer to Ref. Fig. Installation of the Missing X-Fixation Bracket on the LHOver-Head Stowage Compartment Housing Assembly.
3 Torque the screws item 6 to 2.50 Nm (22.126 lbf.in.).4 Install the bin on the LH OHSC, refer to Ref. AMM Task 25-24-41-400-802.
A318/A319/A320/A321SERVICE BULLETIN
Figure ICN-A320-A-25XX1BQB-A-FAPE3-01DME-A-001-01 SHEET 1/2REV 00 Sep 18/19 A320-25-1BQBInstallation of the Missing X-Fixation Bracket on the LH
Over-Head Stowage Compartment Housing Assembly Page 120
CONF 002
B
VIEW SHOWN WITHOUT BINSTYPICAL
ATYPICAL
VIEW LOOKING AFT
C
HOUSING
C
A
A
A
A
B
A
- Z230 Z250
ICN-A320-A-25XX1BQB-A-FAPE3-01DME-A-001-01
A318/A319/A320/A321SERVICE BULLETIN
Figure ICN-A320-A-25XX1BQB-A-FAPE3-01DMF-A-001-01 SHEET 2/2REV 00 Sep 18/19 A320-25-1BQBInstallation of the Missing X-Fixation Bracket on the LH
Over-Head Stowage Compartment Housing Assembly Page 121
CONF 002
TYPICAL
HOUSING
VIEW LOOKING DOWN
AA FWD
CLEARANCE2 mm
(0.079 in)
X-FIXATION BRACKETX-FIXATION BRACKET
BIN
HOUSING
67
1
C
ICN-A320-A-25XX1BQB-A-FAPE3-01DMF-A-001-01
A318/A319/A320/A321SERVICE BULLETIN
REV 00 Sep 18/19 A320-25-1BQBPage 122
CONF 001(4) Task A320-A-25-XX-1BQB-04001-600A-A - Install the Missing X-Fixation
Bracket on the RH OHSC Housing AssemblyJob Set-Up Information
Working Area
Impacted Zone Access / Work Location230 Work location From Frame 21 to Frame 35240 Work location From Frame 35 to Frame 47250 Work location From Frame 47 to Frame 63
Manpower/Resources/Skills
Man-hours 0.25 hMinimum Number of person 1Elapsed Time 0.25 hSkills Cabin
Material necessary to do the jobComponentsITEM PART No. QTY (UM) KEYWORD DRAWING SEE NOTES2 606A00305-001 1 BRACKET (1)6 NAS1801-08-5 4 SCREW (1)7 NAS1149CN832R 4 WASHER (1)NOTE(S)(1): The components listed above are not an AIRBUS Kit, the required parts must be
ordered as necessary through the given channel.
Referenced Information
Manuals/Drawings References/Sheets
AMM06-20-00, Page Block 00106-31-53, Page Block 001Task 20-21-11-911-001Task 25-24-41-400-802
Procedure(a) Standard Practices
1 For the identification of zones, refer to Ref. AMM 06-20-00, Page Block 001.2 For the Frame (FR) identification, refer to Ref. AMM 06-31-53, Page Block
001.3 Tag all the parts you must remove and retain to make the subsequent
installation easier.4 Put all the retained hardware in identified plastic bags and attach the bags
to the related unit.5 To torque tighten the standard threaded fasteners, refer to Ref. AMM Task
20-21-11-911-001.(b) Install the missing x-fixation bracket on the RH OHSC housing.
Refer to Ref. Fig. Installation of the Missing X-Fixation Bracket on the RH Over-Head Stowage Compartment Housing Assembly
A318/A319/A320/A321SERVICE BULLETIN
REV 00 Sep 18/19 A320-25-1BQBPage 123
1 Install:Refer to Ref. Fig. Installation of the Missing X-Fixation Bracket on the RHOver-Head Stowage Compartment Housing Assembly
1 BRACKET 606A00305-001 Item 2with
4 SCREW NAS1801-08-5 Item 6
4 WASHER NAS1149CN832R Item 72 Make sure that the bracket item 2 is installed in ‘Flight Direction’ on the
housing, in front of the bracket of the bin assembly, to face each other,refer to Ref. Fig. Installation of the Missing X-Fixation Bracket on the RHOver-Head Stowage Compartment Housing Assembly.
3 Torque the screws item 6 to 2.50 Nm (22.126 lbf.in.).4 Install the bin on the RH OHSC, refer to Ref. AMM Task 25-24-41-400-802.
A318/A319/A320/A321SERVICE BULLETIN
Figure ICN-A320-A-25XX1BQB-A-FAPE3-00Y3Q-A-003-01 SHEET 1/2REV 00 Sep 18/19 A320-25-1BQBInstallation of the Missing X-Fixation Bracket on the RH
Over-Head Stowage Compartment Housing Assembly Page 124
CONF 001
ATYPICAL
VIEW LOOKING AFT
B
VIEW SHOWN WITHOUT BINSTYPICAL
HOUSING
C
C
- Z230 Z250
A
A
A
A
A
B
ICN-A320-A-25XX1BQB-A-FAPE3-00Y3Q-A-003-01
A318/A319/A320/A321SERVICE BULLETIN
Figure ICN-A320-A-25XX1BQB-A-FAPE3-01DMB-A-001-01 SHEET 2/2REV 00 Sep 18/19 A320-25-1BQBInstallation of the Missing X-Fixation Bracket on the RH
Over-Head Stowage Compartment Housing Assembly Page 125
CONF 001
TYPICAL
VIEW LOOKING DOWN
AA
C
HOUSING
67
2
CLEARANCE2 mm
(0.079 in)
X-FIXATION BRACKETX-FIXATION BRACKET
BIN
HOUSING
FWD
ICN-A320-A-25XX1BQB-A-FAPE3-01DMB-A-001-01
A318/A319/A320/A321SERVICE BULLETIN
REV 00 Sep 18/19 A320-25-1BQBPage 126
CONF 002(4) Task A320-A-25-XX-1BQB-04002-600A-A - Install the Missing X-Fixation
Bracket on the RH OHSC Housing AssemblyJob Set-Up Information
Working Area
Impacted Zone Access / Work Location230 Work location From Frame 21 to Frame 35.8240 Work location From Frame 35.8 to Frame 47250 Work location From Frame 47 to Frame 64260 Work location From Frame 64 to Frame 66
Manpower/Resources/Skills
Man-hours 0.25 hMinimum Number of person 1Elapsed Time 0.25 hSkills Cabin
Material necessary to do the jobComponentsITEM PART No. QTY (UM) KEYWORD DRAWING SEE NOTES2 606A00305-001 1 BRACKET (1)6 NAS1801-08-5 4 SCREW (1)7 NAS1149CN832R 4 WASHER (1)NOTE(S)(1): The components listed above are not an AIRBUS Kit, the required parts must be
ordered as necessary through the given channel.
Referenced Information
Manuals/Drawings References/Sheets
AMM06-20-00, Page Block 00106-31-53, Page Block 001Task 20-21-11-911-001Task 25-24-41-400-802
Procedure(a) Standard Practices
1 For the identification of zones, refer to Ref. AMM 06-20-00, Page Block 001.2 For the Frame (FR) identification, refer to Ref. AMM 06-31-53, Page Block
001.3 Tag all the parts you must remove and retain to make the subsequent
installation easier.4 Put all the retained hardware in identified plastic bags and attach the bags
to the related unit.5 To torque tighten the standard threaded fasteners, refer to Ref. AMM Task
20-21-11-911-001.
A318/A319/A320/A321SERVICE BULLETIN
REV 00 Sep 18/19 A320-25-1BQBPage 127
(b) Install the missing x-fixation bracket on the RH OHSC housing.Refer to Ref. Fig. Installation of the Missing X-Fixation Bracket on the RH Over-Head Stowage Compartment Housing Assembly1 Install:
Refer to Ref. Fig. Installation of the Missing X-Fixation Bracket on the RHOver-Head Stowage Compartment Housing Assembly
1 BRACKET 606A00305-001 Item 2with
4 SCREW NAS1801-08-5 Item 6
4 WASHER NAS1149CN832R Item 72 Make sure that the bracket item 2 is installed in ‘Flight Direction’ on the
housing, in front of the bracket of the bin assembly, to face each other,refer to Ref. Fig. Installation of the Missing X-Fixation Bracket on the RHOver-Head Stowage Compartment Housing Assembly.
3 Torque the screws item 6 to 2.50 Nm (22.126 lbf.in.).4 Install the bin on the RH OHSC, refer to Ref. AMM Task 25-24-41-400-802.
A318/A319/A320/A321SERVICE BULLETIN
Figure ICN-A320-A-25XX1BQB-A-FAPE3-01DMC-A-002-01 SHEET 1/2REV 00 Sep 18/19 A320-25-1BQBInstallation of the Missing X-Fixation Bracket on the RH
Over-Head Stowage Compartment Housing Assembly Page 128
CONF 002
ATYPICAL
VIEW LOOKING AFT
B
VIEW SHOWN WITHOUT BINSTYPICAL
HOUSING
C
C
B
A
- Z230 Z260
A
A
A
A
ICN-A320-A-25XX1BQB-A-FAPE3-01DMC-A-002-01
A318/A319/A320/A321SERVICE BULLETIN
Figure ICN-A320-A-25XX1BQB-A-FAPE3-01DMD-A-001-01 SHEET 2/2REV 00 Sep 18/19 A320-25-1BQBInstallation of the Missing X-Fixation Bracket on the RH
Over-Head Stowage Compartment Housing Assembly Page 129
CONF 002
TYPICAL
VIEW LOOKING DOWN
AA
C
HOUSING
67
2
CLEARANCE2 mm
(0.079 in)
X-FIXATION BRACKETX-FIXATION BRACKET
BIN
HOUSING
FWD
ICN-A320-A-25XX1BQB-A-FAPE3-01DMD-A-001-01
A318/A319/A320/A321SERVICE BULLETIN
REV 00 Sep 18/19 A320-25-1BQBPage 130
CONF 001(5) Task A320-A-25-XX-1BQB-05001-600A-A - Install the Missing X-Fixation
Bracket on the Special LH OHSC Bin AssemblyJob Set-Up Information
Working Area
Impacted Zone Access / Work Location250 Work location From Frame 63 to Frame 64260 Work location From Frame 64 to Frame 66
Manpower/Resources/Skills
Man-hours 0.25 hMinimum Number of person 1Elapsed Time 0.25 hSkills Cabin
Material necessary to do the jobComponentsITEM PART No. QTY (UM) KEYWORD DRAWING SEE NOTES3 606A00305-004 1 BRACKET (1)7 NAS1149CN832R 4 WASHER (1)8 NAS1801-08-10 4 SCREW (1)NOTE(S)(1): The components listed above are not an AIRBUS Kit, the required parts must be
ordered as necessary through the given channel.
Referenced Information
Manuals/Drawings References/Sheets
AMM06-20-00, Page Block 00106-31-53, Page Block 001Task 20-21-11-911-001Task 25-24-41-000-802
Procedure(a) Standard Practices
1 For the identification of zones, refer to Ref. AMM 06-20-00, Page Block 001.2 For the Frame (FR) identification, refer to Ref. AMM 06-31-53, Page Block
001.3 Tag all the parts you must remove and retain to make the subsequent
installation easier.4 Put all the retained hardware in identified plastic bags and attach the bags
to the related unit.5 To torque tighten the standard threaded fasteners, refer to Ref. AMM Task
20-21-11-911-001.(b) Install the missing x-fixation bracket on LH OHSC bin assembly.
Refer to Ref. Fig. Installation of the Missing X-Fixation Bracket on the Special LHOver-Head Stowage Compartment Bin Assembly
A318/A319/A320/A321SERVICE BULLETIN
REV 00 Sep 18/19 A320-25-1BQBPage 131
1 Remove the bin from the LH OHSC, refer to Ref. AMM Task25-24-41-000-802.
2 Install:Refer to Ref. Fig. Installation of the Missing X-Fixation Bracket on theSpecial LH Over-Head Stowage Compartment Bin Assembly
1 BRACKET 606A00305-004 Item 3with
4 SCREW NAS1801-08-10 Item 8
4 WASHER NAS1149CN832R Item 73 Make sure that the bracket item 3 is installed in ‘Flight Direction’ on the bin
assembly, aft of the bracket of the housing, to face each other, refer to Ref.Fig. Installation of the Missing X-Fixation Bracket on the Special LH Over-Head Stowage Compartment Bin Assembly.
4 Torque the screws item 8 to 2.50 Nm (22.126 lbf.in.).
A318/A319/A320/A321SERVICE BULLETIN
Figure ICN-A320-A-25XX1BQB-A-FAPE3-00YK4-A-003-01 SHEET 1/2REV 00 Sep 18/19 A320-25-1BQBInstallation of the Missing X-Fixation Bracket on the Special
LH Over-Head Stowage Compartment Bin Assembly Page 132
CONF 001
A
A
TYPICALVIEW SHOWN WITHOUT HOUSING
B
A
A
BIN
- Z250 Z260
FR69
AFT PAX DOOR
FR66
FR63
B
C
ICN-A320-A-25XX1BQB-A-FAPE3-00YK4-A-003-01
A318/A319/A320/A321SERVICE BULLETIN
Figure ICN-A320-A-25XX1BQB-A-FAPE3-01DMH-A-001-01 SHEET 2/2REV 00 Sep 18/19 A320-25-1BQBInstallation of the Missing X-Fixation Bracket on the Special
LH Over-Head Stowage Compartment Bin Assembly Page 133
CONF 001
87
3
C
BIN
AAFWD
VIEW LOOKING DOWN
X-FIXATION BRACKETX-FIXATION BRACKET
HOUSINGCLEARANCE
2 mm(0.079 in)
BIN
ICN-A320-A-25XX1BQB-A-FAPE3-01DMH-A-001-01
A318/A319/A320/A321SERVICE BULLETIN
REV 00 Sep 18/19 A320-25-1BQBPage 134
CONF 002(5) Task A320-A-25-XX-1BQB-05002-600A-A - Install the Missing X-Fixation
Bracket on the Special LH OHSC Bin AssemblyJob Set-Up Information
Working Area
Impacted Zone Access / Work Location250 Work location From Frame 63 to Frame 64260 Work location From Frame 64 to Frame 66
Manpower/Resources/Skills
Man-hours 0.25 hMinimum Number of person 1Elapsed Time 0.25 hSkills Cabin
Material necessary to do the jobComponentsITEM PART No. QTY (UM) KEYWORD DRAWING SEE NOTES3 606A00305-004 1 BRACKET (1)7 NAS1149CN832R 4 WASHER (1)8 NAS1801-08-10 4 SCREW (1)NOTE(S)(1): The components listed above are not an AIRBUS Kit, the required parts must be
ordered as necessary through the given channel.
Referenced Information
Manuals/Drawings References/Sheets
AMM06-20-00, Page Block 00106-31-53, Page Block 001Task 20-21-11-911-001Task 25-24-41-000-802
Procedure(a) Standard Practices
1 For the identification of zones, refer to Ref. AMM 06-20-00, Page Block 001.2 For the Frame (FR) identification, refer to Ref. AMM 06-31-53, Page Block
001.3 Tag all the parts you must remove and retain to make the subsequent
installation easier.4 Put all the retained hardware in identified plastic bags and attach the bags
to the related unit.5 To torque tighten the standard threaded fasteners, refer to Ref. AMM Task
20-21-11-911-001.(b) Install the missing x-fixation bracket on LH OHSC bin assembly.
Refer to Ref. Fig. Installation of the Missing X-Fixation Bracket on the Special LHOver-Head Stowage Compartment Bin Assembly
A318/A319/A320/A321SERVICE BULLETIN
REV 00 Sep 18/19 A320-25-1BQBPage 135
1 Remove the bin from the LH OHSC, refer to Ref. AMM Task25-24-41-000-802.
2 Install:Refer to Ref. Fig. Installation of the Missing X-Fixation Bracket on theSpecial LH Over-Head Stowage Compartment Bin Assembly
1 BRACKET 606A00305-004 Item 3with
4 SCREW NAS1801-08-10 Item 8
4 WASHER NAS1149CN832R Item 73 Make sure that the bracket item 3 is installed in ‘Flight Direction’ on the bin
assembly, aft of the bracket of the housing, to face each other, refer to Ref.Fig. Installation of the Missing X-Fixation Bracket on the Special LH Over-Head Stowage Compartment Bin Assembly.
4 Torque the screws item 8 to 2.50 Nm (22.126 lbf.in.).
A318/A319/A320/A321SERVICE BULLETIN
Figure ICN-A320-A-25XX1BQB-A-FAPE3-00YK6-A-003-01 SHEET 1/2REV 00 Sep 18/19 A320-25-1BQBInstallation of the Missing X-Fixation Bracket on the Special
LH Over-Head Stowage Compartment Bin Assembly Page 136
CONF 002
A
TYPICALVIEW SHOWN WITHOUT HOUSING
B
A
A
BIN
FR69
AFT PAX DOOR
FR66
FR63
B
A
- Z250 Z260
C
ICN-A320-A-25XX1BQB-A-FAPE3-00YK6-A-003-01
A318/A319/A320/A321SERVICE BULLETIN
Figure ICN-A320-A-25XX1BQB-A-FAPE3-01DMJ-A-001-01 SHEET 2/2REV 00 Sep 18/19 A320-25-1BQBInstallation of the Missing X-Fixation Bracket on the Special
LH Over-Head Stowage Compartment Bin Assembly Page 137
CONF 002
AAFWD
VIEW LOOKING DOWN
C
87
3
BIN
X-FIXATION BRACKETX-FIXATION BRACKET
HOUSINGCLEARANCE
2 mm(0.079 in)
BIN
ICN-A320-A-25XX1BQB-A-FAPE3-01DMJ-A-001-01
A318/A319/A320/A321SERVICE BULLETIN
REV 00 Sep 18/19 A320-25-1BQBPage 138
CONF 001(6) Task A320-A-25-XX-1BQB-06001-600A-A - Install the Missing X-Fixation
Bracket on the Special RH OHSC Bin AssemblyJob Set-Up Information
Working Area
Impacted Zone Access / Work Location250 Work location From Frame 63 to Frame 64260 Work location From Frame 64 to Frame 66
Manpower/Resources/Skills
Man-hours 0.25 hMinimum Number of person 1Elapsed Time 0.25 hSkills Cabin
Material necessary to do the jobComponentsITEM PART No. QTY (UM) KEYWORD DRAWING SEE NOTES4 606A00305-005 1 BRACKET (1)7 NAS1149CN832R 4 WASHER (1)8 NAS1801-08-10 4 SCREW (1)NOTE(S)(1): The components listed above are not an AIRBUS Kit, the required parts must be
ordered as necessary through the given channel.
Referenced Information
Manuals/Drawings References/Sheets
AMM06-20-00, Page Block 00106-31-53, Page Block 001Task 20-21-11-911-001Task 25-24-41-000-802
Procedure(a) Standard Practices
1 For the identification of zones, refer to Ref. AMM 06-20-00, Page Block 001.2 For the Frame (FR) identification, refer to Ref. AMM 06-31-53, Page Block
001.3 Tag all the parts you must remove and retain to make the subsequent
installation easier.4 Put all the retained hardware in identified plastic bags and attach the bags
to the related unit.5 To torque tighten the standard threaded fasteners, refer to Ref. AMM Task
20-21-11-911-001.(b) Install the missing x-fixation bracket on RH OHSC bin assembly.
Refer to Ref. Fig. Installation of the Missing X-Fixation Bracket on the Special RHOver-Head Stowage Compartment Bin Assembly
A318/A319/A320/A321SERVICE BULLETIN
REV 00 Sep 18/19 A320-25-1BQBPage 139
1 Remove the bin from the RH OHSC, refer to Ref. AMM Task25-24-41-000-802.
2 Install:Refer to Ref. Fig. Installation of the Missing X-Fixation Bracket on theSpecial RH Over-Head Stowage Compartment Bin Assembly
1 BRACKET 606A00305-005 Item 4with
4 SCREW NAS1801-08-10 Item 8
4 WASHER NAS1149CN832R Item 73 Make sure that the bracket item 4 is installed in ‘Flight Direction’ on the bin
assembly, aft of the bracket of the housing, to face each other, refer to Ref.Fig. Installation of the Missing X-Fixation Bracket on the Special RH Over-Head Stowage Compartment Bin Assembly.
4 Torque the screws item 8 to 2.50 Nm (22.126 lbf.in.).
A318/A319/A320/A321SERVICE BULLETIN
Figure ICN-A320-A-25XX1BQB-A-FAPE3-00YK5-A-003-01 SHEET 1/2REV 00 Sep 18/19 A320-25-1BQBInstallation of the Missing X-Fixation Bracket on the Special
RH Over-Head Stowage Compartment Bin Assembly Page 140
CONF 001
A
FR69
AFT PAX DOOR
FR66
FR63
B
TYPICALVIEW SHOWN WITHOUT HOUSING
B
A
A
BIN
A
- Z250 Z260
C
ICN-A320-A-25XX1BQB-A-FAPE3-00YK5-A-003-01
A318/A319/A320/A321SERVICE BULLETIN
Figure ICN-A320-A-25XX1BQB-A-FAPE3-01DMI-A-001-01 SHEET 2/2REV 00 Sep 18/19 A320-25-1BQBInstallation of the Missing X-Fixation Bracket on the Special
RH Over-Head Stowage Compartment Bin Assembly Page 141
CONF 001
C
AAVIEW LOOKING DOWN
87
4
BIN
X-FIXATION BRACKETX-FIXATION BRACKET
HOUSINGCLEARANCE
2 mm(0.079 in)
BIN
FWD
ICN-A320-A-25XX1BQB-A-FAPE3-01DMI-A-001-01
A318/A319/A320/A321SERVICE BULLETIN
REV 00 Sep 18/19 A320-25-1BQBPage 142
(7) Task A320-A-25-XX-1BQB-07001-600A-A - Install the Missing X-FixationBracket with Fixation Holder on the LH OHSC Housing AssemblyJob Set-Up Information
Working Area
Impacted Zone Access / Work Location250 Work location From Frame 63 to Frame 64260 Work location From Frame 64 to Frame 66
Manpower/Resources/Skills
Man-hours 0.25 hMinimum Number of person 1Elapsed Time 0.25 hSkills Cabin
Material necessary to do the jobComponentsITEM PART No. QTY (UM) KEYWORD DRAWING SEE NOTES1 606A00305-000 1 BRACKET (1)7 NAS1149CN832R 4 WASHER (1)9 NAS1801-08-7 4 SCREW (1)10 MS21042-08 4 NUT (1)11 606A00095-002 1 HOLDER (1)NOTE(S)(1): The components listed above are not an AIRBUS Kit, the required parts must be
ordered as necessary through the given channel.
Referenced Information
Manuals/Drawings References/Sheets
AMM
06-20-00, Page Block 00106-31-53, Page Block 001Task 20-21-11-911-001Task 23-73-45-000-001Task 23-73-45-400-001Task 25-24-41-400-802Task 25-25-11-000-001Task 25-25-11-400-001
Procedure(a) Standard Practices
1 For the identification of zones, refer to Ref. AMM 06-20-00, Page Block 001.2 For the Frame (FR) identification, refer to Ref. AMM 06-31-53, Page Block
001.3 Tag all the parts you must remove and retain to make the subsequent
installation easier.4 Put all the retained hardware in identified plastic bags and attach the bags
to the related unit.
A318/A319/A320/A321SERVICE BULLETIN
REV 00 Sep 18/19 A320-25-1BQBPage 143
5 To torque tighten the standard threaded fasteners, refer to Ref. AMM Task20-21-11-911-001.
(b) Install the missing x-fixation bracket on the LH OHSC housing.Refer to Ref. Fig. Installation of the Missing X-Fixation Bracket with Holder on theLH Over-Head Stowage Compartment Housing Assembly1 Remove the Passenger Service Unit (PSU), refer to Ref. AMM Task
23-73-45-000-001.2 Remove the filler panels, as necessary, refer to Ref. AMM Task
25-25-11-000-001.3 Install:
Refer to Ref. Fig. Installation of the Missing X-Fixation Bracket with Holderon the LH Over-Head Stowage Compartment Housing Assembly
1 BRACKET 606A00305-000 Item 1with
4 SCREW NAS1801-08-7 Item 9
4 WASHER NAS1149CN832R Item 7
1 HOLDER 606A00095-002 Item 11
4 NUT MS21042-08 Item 104 Make sure that the bracket item 1 is installed in ‘Flight Direction’ on the
housing, in front of the bracket of the bin assembly, to face each other,refer to Ref. Fig. Installation of the Missing X-Fixation Bracket with Holderon the LH Over-Head Stowage Compartment Housing Assembly.
5 Torque the nuts item 10 to 2.50 Nm (22.126 lbf.in.).6 Install the bin on the LH OHSC, refer to Ref. AMM Task 25-24-41-400-802.7 Install the filler panels, if removed, refer to Ref. AMM Task
25-25-11-400-001.8 Install the PSU, refer to Ref. AMM Task 23-73-45-400-001.
A318/A319/A320/A321SERVICE BULLETIN
Figure ICN-A320-A-25XX1BQB-A-FAPE3-00YK7-A-002-01 SHEET 1/2REV 00 Sep 18/19 A320-25-1BQBInstallation of the Missing X-Fixation Bracket with Holder on
the LH Over-Head Stowage Compartment Housing Assembly Page 144
CONF 001
A
FR69
AFT PAX DOOR
FR66
FR63
B
FWD
VIEW LOOKING OUTBOARD
A A
HOUSING
VIEW SHOWN WITHOUT BIN
B
A
- Z250 Z260
C
ICN-A320-A-25XX1BQB-A-FAPE3-00YK7-A-002-01
A318/A319/A320/A321SERVICE BULLETIN
Figure ICN-A320-A-25XX1BQB-A-FAPE3-00YK8-A-003-01 SHEET 2/2REV 00 Sep 18/19 A320-25-1BQBInstallation of the Missing X-Fixation Bracket with Holder on
the LH Over-Head Stowage Compartment Housing Assembly Page 145
CONF 001
97
10
1
11
AAVIEW LOOKING DOWN
FWD
X-FIXATION BRACKETX-FIXATION BRACKET
BIN
HOUSING
CLEARANCE2 mm
(0.079 in)
C
ICN-A320-A-25XX1BQB-A-FAPE3-00YK8-A-003-01
A318/A319/A320/A321SERVICE BULLETIN
REV 00 Sep 18/19 A320-25-1BQBPage 146
CONF 002(7) Task A320-A-25-XX-1BQB-07002-600A-A - Install the Missing X-Fixation
Bracket with Fixation Holder on the LH OHSC Housing AssemblyJob Set-Up Information
Working Area
Impacted Zone Access / Work Location250 Work location From Frame 63 to Frame 64260 Work location From Frame 64 to Frame 66
Manpower/Resources/Skills
Man-hours 0.25 hMinimum Number of person 1Elapsed Time 0.25 hSkills Cabin
Material necessary to do the jobComponentsITEM PART No. QTY (UM) KEYWORD DRAWING SEE NOTES1 606A00305-000 1 BRACKET (1)7 NAS1149CN832R 4 WASHER (1)9 NAS1801-08-7 4 SCREW (1)10 MS21042-08 4 NUT (1)11 606A00095-002 1 HOLDER (1)NOTE(S)(1): The components listed above are not an AIRBUS Kit, the required parts must be
ordered as necessary through the given channel.
Referenced Information
Manuals/Drawings References/Sheets
AMM
06-20-00, Page Block 00106-31-53, Page Block 001Task 20-21-11-911-001Task 23-73-45-000-001Task 23-73-45-400-001Task 25-24-41-400-802Task 25-25-11-000-001Task 25-25-11-400-001
Procedure(a) Standard Practices
1 For the identification of zones, refer to Ref. AMM 06-20-00, Page Block 001.2 For the Frame (FR) identification, refer to Ref. AMM 06-31-53, Page Block
001.3 Tag all the parts you must remove and retain to make the subsequent
installation easier.4 Put all the retained hardware in identified plastic bags and attach the bags
to the related unit.
A318/A319/A320/A321SERVICE BULLETIN
REV 00 Sep 18/19 A320-25-1BQBPage 147
5 To torque tighten the standard threaded fasteners, refer to Ref. AMM Task20-21-11-911-001.
(b) Install the missing x-fixation bracket on the LH OHSC housing.Refer to Ref. Fig. Installation of the Missing X-Fixation Bracket with Holder on theLH Over-Head Stowage Compartment Housing Assembly1 Remove the Passenger Service Unit (PSU), refer to Ref. AMM Task
23-73-45-000-001.2 Remove the filler panels, as necessary, refer to Ref. AMM Task
25-25-11-000-001.3 Install:
Refer to Ref. Fig. Installation of the Missing X-Fixation Bracket with Holderon the LH Over-Head Stowage Compartment Housing Assembly
1 BRACKET 606A00305-000 Item 1with
4 SCREW NAS1801-08-7 Item 9
4 WASHER NAS1149CN832R Item 7
1 HOLDER 606A00095-002 Item 11
4 NUT MS21042-08 Item 104 Make sure that the bracket item 1 is installed in ‘Flight Direction’ on the
housing, in front of the bracket of the bin assembly, to face each other,refer to Ref. Fig. Installation of the Missing X-Fixation Bracket with Holderon the LH Over-Head Stowage Compartment Housing Assembly.
5 Torque the nuts item 10 to 2.50 Nm (22.126 lbf.in.).6 Install the bin on the LH OHSC, refer to Ref. AMM Task 25-24-41-400-802.7 Install the filler panels, if removed, refer to Ref. AMM Task
25-25-11-400-001.8 Install the PSU, refer to Ref. AMM Task 23-73-45-400-001.
A318/A319/A320/A321SERVICE BULLETIN
Figure ICN-A320-A-25XX1BQB-A-FAPE3-00YNQ-A-002-01 SHEET 1/2REV 00 Sep 18/19 A320-25-1BQBInstallation of the Missing X-Fixation Bracket with Holder on
the LH Over-Head Stowage Compartment Housing Assembly Page 148
CONF 002
FWD
VIEW LOOKING OUTBOARD
A A
HOUSING
VIEW SHOWN WITHOUT BIN
A
FR69
AFT PAX DOOR
FR66
FR63
B
A
- Z250 Z260
B
C
ICN-A320-A-25XX1BQB-A-FAPE3-00YNQ-A-002-01
A318/A319/A320/A321SERVICE BULLETIN
Figure ICN-A320-A-25XX1BQB-A-FAPE3-00YNR-A-003-01 SHEET 2/2REV 00 Sep 18/19 A320-25-1BQBInstallation of the Missing X-Fixation Bracket with Holder on
the LH Over-Head Stowage Compartment Housing Assembly Page 149
CONF 002
AAVIEW LOOKING DOWN
FWD
X-FIXATION BRACKETX-FIXATION BRACKET
BIN
HOUSING
CLEARANCE2 mm
(0.079 in)
C
97
10
1
11
ICN-A320-A-25XX1BQB-A-FAPE3-00YNR-A-003-01
A318/A319/A320/A321SERVICE BULLETIN
REV 00 Sep 18/19 A320-25-1BQBPage 150
CONF 001(8) Task A320-A-25-XX-1BQB-08001-600A-A - Install the Missing X-Fixation
Bracket with Fixation Holder on the RH OHSC Housing AssemblyJob Set-Up Information
Working Area
Impacted Zone Access / Work Location250 Work location From Frame 63 to Frame 64260 Work location From Frame 64 to Frame 66
Manpower/Resources/Skills
Man-hours 0.25 hMinimum Number of person 1Elapsed Time 0.25 hSkills Cabin
Material necessary to do the jobComponentsITEM PART No. QTY (UM) KEYWORD DRAWING SEE NOTES2 606A00305-001 1 BRACKET (1)7 NAS1149CN832R 4 WASHER (1)9 NAS1801-08-7 4 SCREW (1)10 MS21042-08 4 NUT (1)11 606A00095-002 1 HOLDER (1)NOTE(S)(1): The components listed above are not an AIRBUS Kit, the required parts must be
ordered as necessary through the given channel.
Referenced Information
Manuals/Drawings References/Sheets
AMM
06-20-00, Page Block 00106-31-53, Page Block 001Task 20-21-11-911-001Task 23-73-45-000-001Task 23-73-45-400-001Task 25-24-41-400-802Task 25-25-11-000-001Task 25-25-11-400-001
Procedure(a) Standard Practices
1 For the identification of zones, refer to Ref. AMM 06-20-00, Page Block 001.2 For the Frame (FR) identification, refer to Ref. AMM 06-31-53, Page Block
001.3 Tag all the parts you must remove and retain to make the subsequent
installation easier.4 Put all the retained hardware in identified plastic bags and attach the bags
to the related unit.
A318/A319/A320/A321SERVICE BULLETIN
REV 00 Sep 18/19 A320-25-1BQBPage 151
5 To torque tighten the standard threaded fasteners, refer to Ref. AMM Task20-21-11-911-001.
(b) Install the missing x-fixation bracket on RH OHSC housing.Refer to Ref. Fig. Installation of the Missing X-Fixation Bracket with Holder on theRH Over-Head Stowage Compartment Housing Assembly1 Remove the PSU, refer to Ref. AMM Task 23-73-45-000-001.2 Remove the filler panels, as necessary, refer to Ref. AMM Task
25-25-11-000-001.3 Install:
Refer to Ref. Fig. Installation of the Missing X-Fixation Bracket with Holderon the RH Over-Head Stowage Compartment Housing Assembly
1 BRACKET 606A00305-001 Item 2with
4 SCREW NAS1801-08-7 Item 9
4 WASHER NAS1149CN832R Item 7
1 HOLDER 606A00095-002 Item 11
4 NUT MS21042-08 Item 104 Make sure that the bracket item 2 is installed in ‘Flight Direction’ on the
housing, in front of the bracket of the bin assembly, to face each other,refer to Ref. Fig. Installation of the Missing X-Fixation Bracket with Holderon the RH Over-Head Stowage Compartment Housing Assembly.
5 Torque the nuts item 10 to 2.50 Nm (22.126 lbf.in.).6 Install the bin on the RH OHSC, refer to Ref. AMM Task 25-24-41-400-802.7 Install the filler panels, if removed, refer to Ref. AMM Task
25-25-11-400-001.8 Install the PSU, refer to Ref. AMM Task 23-73-45-400-001.
A318/A319/A320/A321SERVICE BULLETIN
Figure ICN-A320-A-25XX1BQB-A-FAPE3-00YP6-A-003-01 SHEET 1/2REV 00 Sep 18/19 A320-25-1BQBInstallation of the Missing X-Fixation Bracket with Holder on
the RH Over-Head Stowage Compartment Housing Assembly Page 152
CONF 001
A
- Z250 Z260
A
FR69
AFT PAX DOOR
FR66
FR63
B
FWD
HOUSING
A A
VIEW LOOKING OUTBOARDVIEW SHOWN WITHOUT BIN
B
C
ICN-A320-A-25XX1BQB-A-FAPE3-00YP6-A-003-01
A318/A319/A320/A321SERVICE BULLETIN
Figure ICN-A320-A-25XX1BQB-A-FAPE3-00YP7-A-003-01 SHEET 2/2REV 00 Sep 18/19 A320-25-1BQBInstallation of the Missing X-Fixation Bracket with Holder on
the RH Over-Head Stowage Compartment Housing Assembly Page 153
CONF 001
AAVIEW LOOKING DOWN
C
X-FIXATION BRACKETX-FIXATION BRACKET
BIN
HOUSING
CLEARANCE2 mm
(0.079 in)
97
10
1
11
FWD
ICN-A320-A-25XX1BQB-A-FAPE3-00YP7-A-003-01
A318/A319/A320/A321SERVICE BULLETIN
REV 00 Sep 18/19 A320-25-1BQBPage 154
(9) Task A320-A-25-XX-1BQB-09001-600A-A - Remove and Install the X-FixationBracket in the Correct Position on the LH OHSC Bin AssemblyJob Set-Up Information
Working Area
Impacted Zone Access / Work Location230 Work location From Frame 21 to Frame 35240 Work location From Frame 35 to Frame 47250 Work location From Frame 47 to Frame 63
Manpower/Resources/Skills
Man-hours 0.25 hMinimum Number of person 1Elapsed Time 0.25 hSkills Cabin
Referenced Information
Manuals/Drawings References/Sheets
AMM06-20-00, Page Block 00106-31-53, Page Block 001Task 20-21-11-911-001Task 25-24-41-000-802
Procedure(a) Standard Practices
1 For the identification of zones, refer to Ref. AMM 06-20-00, Page Block 001.2 For the Frame (FR) identification, refer to Ref. AMM 06-31-53, Page Block
001.3 Tag all the parts you must remove and retain to make the subsequent
installation easier.4 Put all the retained hardware in identified plastic bags and attach the bags
to the related unit.5 To torque tighten the standard threaded fasteners, refer to Ref. AMM Task
20-21-11-911-001.(b) Remove and install the x-fixation bracket in the correct position on the LH OHSC
bin assembly.Refer to Ref. Fig. Remove and Install the X-fixation Bracket in the Correct Positionon the LH Over-Head Stowage Compartment Bin Assembly1 Remove the bin from the LH OHSC, refer to Ref. AMM Task
25-24-41-000-802.2 Remove:
Refer to Ref. Fig. Remove and Install the X-fixation Bracket in the CorrectPosition on the LH Over-Head Stowage Compartment Bin Assembly
4 SCREW Item (6) Retain
4 WASHER Item (7) Retain
1 BRACKET Item (1) Retain
A318/A319/A320/A321SERVICE BULLETIN
REV 00 Sep 18/19 A320-25-1BQBPage 155
3 Install:Refer to Ref. Fig. Remove and Install the X-fixation Bracket in the CorrectPosition on the LH Over-Head Stowage Compartment Bin Assembly
1 BRACKET Item (1) Retainedwith
4 WASHER Item (7) Retained
4 SCREW Item (6) Retained4 Make sure that the bracket item (1) is installed in ‘Flight Direction’ on the
bin assembly, aft of the bracket of the housing, to face each other, refer toRef. Fig. Remove and Install the X-fixation Bracket in the Correct Position onthe LH Over-Head Stowage Compartment Bin Assembly.
5 Torque the screws item (6) to 2.50 Nm (22.126 lbf.in.).
A318/A319/A320/A321SERVICE BULLETIN
Figure ICN-A320-A-25XX1BQB-A-FAPE3-00YP8-A-003-01 SHEET 1/2REV 00 Sep 18/19 A320-25-1BQBRemove and Install the X-fixation Bracket
in the Correct Position on the LH Over-Head Stowage Compartment Bin Assembly Page 156
CONF 001
- Z230 Z250
A
ATYPICAL
VIEW LOOKING AFT
TYPICALVIEW SHOWN WITHOUT HOUSING
B
A
A
BIN
C
B
ICN-A320-A-25XX1BQB-A-FAPE3-00YP8-A-003-01
A318/A319/A320/A321SERVICE BULLETIN
Figure ICN-A320-A-25XX1BQB-A-FAPE3-01DMP-A-001-01 SHEET 2/2REV 00 Sep 18/19 A320-25-1BQBRemove and Install the X-fixation Bracket
in the Correct Position on the LH Over-Head Stowage Compartment Bin Assembly Page 157
CONF 001
(6)(7)
(1)
C
AAFWD
VIEW LOOKING DOWN
CLEARANCE2 mm
(0.079 in)
X-FIXATION BRACKETX-FIXATION BRACKET
HOUSING
BIN
BIN
ICN-A320-A-25XX1BQB-A-FAPE3-01DMP-A-001-01
A318/A319/A320/A321SERVICE BULLETIN
REV 00 Sep 18/19 A320-25-1BQBPage 158
CONF 002(9) Task A320-A-25-XX-1BQB-09002-600A-A - Remove and Install the X-Fixation
Bracket in the Correct Position on the LH OHSC Bin AssemblyJob Set-Up Information
Working Area
Impacted Zone Access / Work Location230 Work location From Frame 21 to Frame 35.8240 Work location From Frame 35.8 to Frame 47250 Work location From Frame 47 to Frame 63
Manpower/Resources/Skills
Man-hours 0.25 hMinimum Number of person 1Elapsed Time 0.25 hSkills Cabin
Referenced Information
Manuals/Drawings References/Sheets
AMM06-20-00, Page Block 00106-31-53, Page Block 001Task 20-21-11-911-001Task 25-24-41-000-802
Procedure(a) Standard Practices
1 For the identification of zones, refer to Ref. AMM 06-20-00, Page Block 001.2 For the Frame (FR) identification, refer to Ref. AMM 06-31-53, Page Block
001.3 Tag all the parts you must remove and retain to make the subsequent
installation easier.4 Put all the retained hardware in identified plastic bags and attach the bags
to the related unit.5 To torque tighten the standard threaded fasteners, refer to Ref. AMM Task
20-21-11-911-001.(b) Remove and install the x-fixation bracket in the correct position on the LH OHSC
bin assembly.Refer to Ref. Fig. Remove and Install the X-fixation Bracket in the Correct Positionon the LH Over-Head Stowage Compartment Bin Assembly1 Remove the bin from the LH OHSC, refer to Ref. AMM Task
25-24-41-000-802.2 Remove:
Refer to Ref. Fig. Remove and Install the X-fixation Bracket in the CorrectPosition on the LH Over-Head Stowage Compartment Bin Assembly
4 SCREW Item (6) Retain
4 WASHER Item (7) Retain
A318/A319/A320/A321SERVICE BULLETIN
REV 00 Sep 18/19 A320-25-1BQBPage 159
1 BRACKET Item (1) Retain3 Install:
Refer to Ref. Fig. Remove and Install the X-fixation Bracket in the CorrectPosition on the LH Over-Head Stowage Compartment Bin Assembly
1 BRACKET Item (1) Retainedwith
4 WASHER Item (7) Retained
4 SCREW Item (6) Retained4 Make sure that the bracket item (1) is installed in ‘Flight Direction’ on the
bin assembly, aft of the bracket of the housing, to face each other, refer toRef. Fig. Remove and Install the X-fixation Bracket in the Correct Position onthe LH Over-Head Stowage Compartment Bin Assembly.
5 Torque the screws item (6) to 2.50 Nm (22.126 lbf.in.).
A318/A319/A320/A321SERVICE BULLETIN
Figure ICN-A320-A-25XX1BQB-A-FAPE3-01DMK-A-001-01 SHEET 1/2REV 00 Sep 18/19 A320-25-1BQBRemove and Install the X-fixation Bracket
in the Correct Position on the LH Over-Head Stowage Compartment Bin Assembly Page 160
CONF 002
ATYPICAL
VIEW LOOKING AFT
TYPICALVIEW SHOWN WITHOUT HOUSING
B
A
A
BIN
C
B
A
- Z230 Z250
ICN-A320-A-25XX1BQB-A-FAPE3-01DMK-A-001-01
A318/A319/A320/A321SERVICE BULLETIN
Figure ICN-A320-A-25XX1BQB-A-FAPE3-01DML-A-001-01 SHEET 2/2REV 00 Sep 18/19 A320-25-1BQBRemove and Install the X-fixation Bracket
in the Correct Position on the LH Over-Head Stowage Compartment Bin Assembly Page 161
CONF 002
(6)
(1)
C
AAFWD
VIEW LOOKING DOWN
CLEARANCE2 mm
(0.079 in)
X-FIXATION BRACKETX-FIXATION BRACKET
HOUSING
BIN
BIN
(7)
ICN-A320-A-25XX1BQB-A-FAPE3-01DML-A-001-01
A318/A319/A320/A321SERVICE BULLETIN
REV 00 Sep 18/19 A320-25-1BQBPage 162
CONF 001(10) Task A320-A-25-XX-1BQB-10001-600A-A - Remove and Install the X-Fixation
Bracket in the Correct Position on the RH OHSC Bin AssemblyJob Set-Up Information
Working Area
Impacted Zone Access / Work Location230 Work location From Frame 21 to Frame 35240 Work location From Frame 35 to Frame 47250 Work location From Frame 47 to Frame 63
Manpower/Resources/Skills
Man-hours 0.25 hMinimum Number of person 1Elapsed Time 0.25 hSkills Cabin
Referenced Information
Manuals/Drawings References/Sheets
AMM06-20-00, Page Block 00106-31-53, Page Block 001Task 20-21-11-911-001Task 25-24-41-000-802
Procedure(a) Standard Practices
1 For the identification of zones, refer to Ref. AMM 06-20-00, Page Block 001.2 For the Frame (FR) identification, refer to Ref. AMM 06-31-53, Page Block
001.3 Tag all the parts you must remove and retain to make the subsequent
installation easier.4 Put all the retained hardware in identified plastic bags and attach the bags
to the related unit.5 To torque tighten the standard threaded fasteners, refer to Ref. AMM Task
20-21-11-911-001.(b) Remove and install the x-fixation bracket in the correct position on the RH OHSC
bin assembly.Refer to Ref. Fig. Remove and Install the X-fixation Bracket in the Correct Positionon the RH Over-Head Stowage Compartment Bin Assembly1 Remove the bin from the RH OHSC, refer to Ref. AMM Task
25-24-41-000-802.2 Remove:
Refer to Ref. Fig. Remove and Install the X-fixation Bracket in the CorrectPosition on the RH Over-Head Stowage Compartment Bin Assembly
4 SCREW Item (6) Retain
4 WASHER Item (7) Retain
A318/A319/A320/A321SERVICE BULLETIN
REV 00 Sep 18/19 A320-25-1BQBPage 163
1 BRACKET Item (2) Retain3 Install:
Refer to Ref. Fig. Remove and Install the X-fixation Bracket in the CorrectPosition on the RH Over-Head Stowage Compartment Bin Assembly
1 BRACKET Item (2) Retainedwith
4 WASHER Item (7) Retained
4 SCREW Item (6) Retained4 Make sure that the bracket item (2) is installed in ‘Flight Direction’ on the
bin assembly, aft of the bracket of the housing, to face each other, refer toRef. Fig. Remove and Install the X-fixation Bracket in the Correct Position onthe RH Over-Head Stowage Compartment Bin Assembly.
5 Torque the screws item (6) to 2.50 Nm (22.126 lbf.in.).
A318/A319/A320/A321SERVICE BULLETIN
Figure ICN-A320-A-25XX1BQB-A-FAPE3-00YP9-A-003-01 SHEET 1/2REV 00 Sep 18/19 A320-25-1BQBRemove and Install the X-fixation Bracket
in the Correct Position on the RH Over-Head Stowage Compartment Bin Assembly Page 164
CONF 001
- Z230 Z250
A
ATYPICAL
VIEW LOOKING AFT
TYPICALVIEW SHOWN WITHOUT HOUSING
B
A
A
BIN
C
B
ICN-A320-A-25XX1BQB-A-FAPE3-00YP9-A-003-01
A318/A319/A320/A321SERVICE BULLETIN
Figure ICN-A320-A-25XX1BQB-A-FAPE3-01DMO-A-001-01 SHEET 2/2REV 00 Sep 18/19 A320-25-1BQBRemove and Install the X-fixation Bracket
in the Correct Position on the RH Over-Head Stowage Compartment Bin Assembly Page 165
CONF 001
(2)
(7)
(6)
C
AAVIEW LOOKING DOWN
CLEARANCE2 mm
(0.079 in)
X-FIXATION BRACKETX-FIXATION BRACKET
HOUSING
BIN
FWD
BIN
ICN-A320-A-25XX1BQB-A-FAPE3-01DMO-A-001-01
A318/A319/A320/A321SERVICE BULLETIN
REV 00 Sep 18/19 A320-25-1BQBPage 166
CONF 002(10) Task A320-A-25-XX-1BQB-10002-600A-A - Remove and Install the X-Fixation
Bracket in the Correct Position on the RH OHSC Bin AssemblyJob Set-Up Information
Working Area
Impacted Zone Access / Work Location230 Work location From Frame 21 to Frame 35.8240 Work location From Frame 35.8 to Frame 47250 Work location From Frame 47 to Frame 64260 Work location From Frame 64 to Frame 66
Manpower/Resources/Skills
Man-hours 0.25 hMinimum Number of person 1Elapsed Time 0.25 hSkills Cabin
Referenced Information
Manuals/Drawings References/Sheets
AMM06-20-00, Page Block 00106-31-53, Page Block 001Task 20-21-11-911-001Task 25-24-41-000-802
Procedure(a) Standard Practices
1 For the identification of zones, refer to Ref. AMM 06-20-00, Page Block 001.2 For the Frame (FR) identification, refer to Ref. AMM 06-31-53, Page Block
001.3 Tag all the parts you must remove and retain to make the subsequent
installation easier.4 Put all the retained hardware in identified plastic bags and attach the bags
to the related unit.5 To torque tighten the standard threaded fasteners, refer to Ref. AMM Task
20-21-11-911-001.(b) Remove and install the x-fixation bracket in the correct position on the RH OHSC
bin assembly.Refer to Ref. Fig. Remove and Install the X-fixation Bracket in the Correct Positionon the RH Over-Head Stowage Compartment Bin Assembly1 Remove the bin from the RH OHSC, refer to Ref. AMM Task
25-24-41-000-802.2 Remove:
Refer to Ref. Fig. Remove and Install the X-fixation Bracket in the CorrectPosition on the RH Over-Head Stowage Compartment Bin Assembly
4 SCREW Item (6) Retain
A318/A319/A320/A321SERVICE BULLETIN
REV 00 Sep 18/19 A320-25-1BQBPage 167
4 WASHER Item (7) Retain
1 BRACKET Item (2) Retain3 Install:
Refer to Ref. Fig. Remove and Install the X-fixation Bracket in the CorrectPosition on the RH Over-Head Stowage Compartment Bin Assembly
1 BRACKET Item (2) Retainedwith
4 WASHER Item (7) Retained
4 SCREW Item (6) Retained4 Make sure that the bracket item (2) is installed in ‘Flight Direction’ on the
bin assembly, aft of the bracket of the housing, to face each other, refer toRef. Fig. Remove and Install the X-fixation Bracket in the Correct Position onthe RH Over-Head Stowage Compartment Bin Assembly.
5 Torque the screws item (6) to 2.50 Nm (22.126 lbf.in.).
A318/A319/A320/A321SERVICE BULLETIN
Figure ICN-A320-A-25XX1BQB-A-FAPE3-01DMM-A-002-01 SHEET 1/2REV 00 Sep 18/19 A320-25-1BQBRemove and Install the X-fixation Bracket
in the Correct Position on the RH Over-Head Stowage Compartment Bin Assembly Page 168
CONF 002
ATYPICAL
VIEW LOOKING AFT
TYPICALVIEW SHOWN WITHOUT HOUSING
B
BIN
C
B
A
- Z230 Z260
A
A
ICN-A320-A-25XX1BQB-A-FAPE3-01DMM-A-002-01
A318/A319/A320/A321SERVICE BULLETIN
Figure ICN-A320-A-25XX1BQB-A-FAPE3-01DMN-A-001-01 SHEET 2/2REV 00 Sep 18/19 A320-25-1BQBRemove and Install the X-fixation Bracket
in the Correct Position on the RH Over-Head Stowage Compartment Bin Assembly Page 169
CONF 002
(2)
(7)
(6)
C
AAVIEW LOOKING DOWN
CLEARANCE2 mm
(0.079 in)
X-FIXATION BRACKETX-FIXATION BRACKET
HOUSING
BIN
FWD
BIN
ICN-A320-A-25XX1BQB-A-FAPE3-01DMN-A-001-01
A318/A319/A320/A321SERVICE BULLETIN
REV 00 Sep 18/19 A320-25-1BQBPage 170
CONF 001(11) Task A320-A-25-XX-1BQB-11001-600A-A - Remove and Install the X-Fixation
Bracket in the Correct Position on the LH OHSC Housing AssemblyJob Set-Up Information
Working Area
Impacted Zone Access / Work Location230 Work location From Frame 21 to Frame 35240 Work location From Frame 35 to Frame 47250 Work location From Frame 47 to Frame 63
Manpower/Resources/Skills
Man-hours 0.25 hMinimum Number of person 1Elapsed Time 0.25 hSkills Cabin
Referenced Information
Manuals/Drawings References/Sheets
AMM06-20-00, Page Block 00106-31-53, Page Block 001Task 20-21-11-911-001Task 25-24-41-400-802
Procedure(a) Standard Practices
1 For the identification of zones, refer to Ref. AMM 06-20-00, Page Block 001.2 For the Frame (FR) identification, refer to Ref. AMM 06-31-53, Page Block
001.3 Tag all the parts you must remove and retain to make the subsequent
installation easier.4 Put all the retained hardware in identified plastic bags and attach the bags
to the related unit.5 To torque tighten the standard threaded fasteners, refer to Ref. AMM Task
20-21-11-911-001.(b) Remove and install the x-fixation bracket in the correct position on the LH OHSC
housing.Refer to Ref. Fig. Remove and Install the X-fixation Bracket in the Correct Positionon the LH Over-Head Stowage Compartment Housing Assembly1 Remove:
Refer to Ref. Fig. Remove and Install the X-fixation Bracket in the CorrectPosition on the LH Over-Head Stowage Compartment Housing Assembly
4 SCREW Item (6) Retain
4 WASHER Item (7) Retain
1 BRACKET Item (1) Retain
A318/A319/A320/A321SERVICE BULLETIN
REV 00 Sep 18/19 A320-25-1BQBPage 171
2 Install:Refer to Ref. Fig. Remove and Install the X-fixation Bracket in the CorrectPosition on the LH Over-Head Stowage Compartment Housing Assembly
1 BRACKET Item (1) Retainedwith
4 WASHER Item (7) Retained
4 SCREW Item (6) Retained3 Make sure that the bracket item (1) is installed in ‘Flight Direction’ on the
housing, in front of the bracket of the bin assembly, to face each other,refer to Ref. Fig. Remove and Install the X-fixation Bracket in the CorrectPosition on the LH Over-Head Stowage Compartment Housing Assembly.
4 Torque the screws item (6) to 2.50 Nm (22.126 lbf.in.).5 Install the bin on the LH OHSC, refer to Ref. AMM Task 25-24-41-400-802.
A318/A319/A320/A321SERVICE BULLETIN
Figure ICN-A320-A-25XX1BQB-A-FAPE3-00YPA-A-003-01 SHEET 1/2REV 00 Sep 18/19 A320-25-1BQBRemove and Install the X-fixation Bracket
in the Correct Position on the LH Over-HeadStowage Compartment Housing Assembly Page 172
CONF 001
B
VIEW SHOWN WITHOUT BINSTYPICAL
- Z230 Z250
A
ATYPICAL
VIEW LOOKING AFT
C
HOUSING
C
A
A
A
A
B
ICN-A320-A-25XX1BQB-A-FAPE3-00YPA-A-003-01
A318/A319/A320/A321SERVICE BULLETIN
Figure ICN-A320-A-25XX1BQB-A-FAPE3-01DMU-A-001-01 SHEET 2/2REV 00 Sep 18/19 A320-25-1BQBRemove and Install the X-fixation Bracket
in the Correct Position on the LH Over-HeadStowage Compartment Housing Assembly Page 173
CONF 001
TYPICAL
HOUSING
VIEW LOOKING DOWN
AA FWD
CLEARANCE2 mm
(0.079 in)
X-FIXATION BRACKETX-FIXATION BRACKET
BIN
HOUSING
(6)(7)
(1)
C
ICN-A320-A-25XX1BQB-A-FAPE3-01DMU-A-001-01
A318/A319/A320/A321SERVICE BULLETIN
REV 00 Sep 18/19 A320-25-1BQBPage 174
CONF 002(11) Task A320-A-25-XX-1BQB-11002-600A-A - Remove and Install the X-Fixation
Bracket in the Correct Position on the LH OHSC Housing AssemblyJob Set-Up Information
Working Area
Impacted Zone Access / Work Location230 Work location From Frame 21 to Frame 35.8240 Work location From Frame 35.8 to Frame 47250 Work location From Frame 47 to Frame 63
Manpower/Resources/Skills
Man-hours 0.25 hMinimum Number of person 1Elapsed Time 0.25 hSkills Cabin
Referenced Information
Manuals/Drawings References/Sheets
AMM06-20-00, Page Block 00106-31-53, Page Block 001Task 20-21-11-911-001Task 25-24-41-400-802
Procedure(a) Standard Practices
1 For the identification of zones, refer to Ref. AMM 06-20-00, Page Block 001.2 For the Frame (FR) identification, refer to Ref. AMM 06-31-53, Page Block
001.3 Tag all the parts you must remove and retain to make the subsequent
installation easier.4 Put all the retained hardware in identified plastic bags and attach the bags
to the related unit.5 To torque tighten the standard threaded fasteners, refer to Ref. AMM Task
20-21-11-911-001.(b) Remove and install the x-fixation bracket in the correct position on the LH OHSC
housing.Refer to Ref. Fig. Remove and Install the X-fixation Bracket in the Correct Positionon the LH Over-Head Stowage Compartment Housing Assembly1 Remove:
Refer to Ref. Fig. Remove and Install the X-fixation Bracket in the CorrectPosition on the LH Over-Head Stowage Compartment Housing Assembly
4 SCREW Item (6) Retain
4 WASHER Item (7) Retain
1 BRACKET Item (1) Retain
A318/A319/A320/A321SERVICE BULLETIN
REV 00 Sep 18/19 A320-25-1BQBPage 175
2 Install:Refer to Ref. Fig. Remove and Install the X-fixation Bracket in the CorrectPosition on the LH Over-Head Stowage Compartment Housing Assembly
1 BRACKET Item (1) Retainedwith
4 WASHER Item (7) Retained
4 SCREW Item (6) Retained3 Make sure that the bracket item (1) is installed in ‘Flight Direction’ on the
housing, in front of the bracket of the bin assembly, to face each other,refer to Ref. Fig. Remove and Install the X-fixation Bracket in the CorrectPosition on the LH Over-Head Stowage Compartment Housing Assembly.
4 Torque the screws item (6) to 2.50 Nm (22.126 lbf.in.).5 Install the bin on the LH OHSC, refer to Ref. AMM Task 25-24-41-400-802.
A318/A319/A320/A321SERVICE BULLETIN
Figure ICN-A320-A-25XX1BQB-A-FAPE3-01DMQ-A-001-01 SHEET 1/2REV 00 Sep 18/19 A320-25-1BQBRemove and Install the X-fixation Bracket
in the Correct Position on the LH Over-HeadStowage Compartment Housing Assembly Page 176
CONF 002
B
VIEW SHOWN WITHOUT BINSTYPICAL
ATYPICAL
VIEW LOOKING AFT
C
HOUSING
C
- Z230 Z250
A
A
A
A
A
B
ICN-A320-A-25XX1BQB-A-FAPE3-01DMQ-A-001-01
A318/A319/A320/A321SERVICE BULLETIN
Figure ICN-A320-A-25XX1BQB-A-FAPE3-01DMR-A-001-01 SHEET 2/2REV 00 Sep 18/19 A320-25-1BQBRemove and Install the X-fixation Bracket
in the Correct Position on the LH Over-HeadStowage Compartment Housing Assembly Page 177
CONF 002
TYPICAL
HOUSING
VIEW LOOKING DOWN
AA FWD
CLEARANCE2 mm
(0.079 in)
X-FIXATION BRACKETX-FIXATION BRACKET
BIN
HOUSING
(6)(7)
(1)
C
ICN-A320-A-25XX1BQB-A-FAPE3-01DMR-A-001-01
A318/A319/A320/A321SERVICE BULLETIN
REV 00 Sep 18/19 A320-25-1BQBPage 178
CONF 001(12) Task A320-A-25-XX-1BQB-12001-600A-A - Remove and Install the X-Fixation
Bracket in the Correct Position on the RH OHSC Housing AssemblyJob Set-Up Information
Working Area
Impacted Zone Access / Work Location230 Work location From Frame 21 to Frame 35240 Work location From Frame 35 to Frame 47250 Work location From Frame 47 to Frame 63
Manpower/Resources/Skills
Man-hours 0.25 hMinimum Number of person 1Elapsed Time 0.25 hSkills Cabin
Referenced Information
Manuals/Drawings References/Sheets
AMM06-20-00, Page Block 00106-31-53, Page Block 001Task 20-21-11-911-001Task 25-24-41-400-802
Procedure(a) Standard Practices
1 For the identification of zones, refer to Ref. AMM 06-20-00, Page Block 001.2 For the Frame (FR) identification, refer to Ref. AMM 06-31-53, Page Block
001.3 Tag all the parts you must remove and retain to make the subsequent
installation easier.4 Put all the retained hardware in identified plastic bags and attach the bags
to the related unit.5 To torque tighten the standard threaded fasteners, refer to Ref. AMM Task
20-21-11-911-001.(b) Remove and install the x-fixation bracket in the correct position on the RH OHSC
housing.Refer to Ref. Fig. Remove and Install the X-fixation Bracket in the Correct Positionon the RH Over-Head Stowage Compartment Housing Assembly1 Remove:
Refer to Ref. Fig. Remove and Install the X-fixation Bracket in the CorrectPosition on the RH Over-Head Stowage Compartment Housing Assembly
4 SCREW Item (6) Retain
4 WASHER Item (7) Retain
1 BRACKET Item (2) Retain
A318/A319/A320/A321SERVICE BULLETIN
REV 00 Sep 18/19 A320-25-1BQBPage 179
2 Install:Refer to Ref. Fig. Remove and Install the X-fixation Bracket in the CorrectPosition on the RH Over-Head Stowage Compartment Housing Assembly
1 BRACKET Item (2) Retainedwith
4 WASHER Item (7) Retained
4 SCREW Item (6) Retained3 Make sure that the bracket item (2) is installed in ‘Flight Direction’ on the
housing, in front of the bracket of the bin assembly, to face each other,refer to Ref. Fig. Remove and Install the X-fixation Bracket in the CorrectPosition on the RH Over-Head Stowage Compartment Housing Assembly.
4 Torque the screws item (6) to 2.50 Nm (22.126 lbf.in.).5 Install the bin on the RH OHSC, refer to Ref. AMM Task 25-24-41-400-802.
A318/A319/A320/A321SERVICE BULLETIN
Figure ICN-A320-A-25XX1BQB-A-FAPE3-00YPB-A-003-01 SHEET 1/2REV 00 Sep 18/19 A320-25-1BQBRemove and Install the X-fixation Bracket in
the Correct Position on the RH Over-HeadStowage Compartment Housing Assembly Page 180
CONF 001
ATYPICAL
VIEW LOOKING AFT
B
VIEW SHOWN WITHOUT BINSTYPICAL
HOUSING
C
C
- Z230 Z250
A
A
A
A
A
B
ICN-A320-A-25XX1BQB-A-FAPE3-00YPB-A-003-01
A318/A319/A320/A321SERVICE BULLETIN
Figure ICN-A320-A-25XX1BQB-A-FAPE3-01DMV-A-001-01 SHEET 2/2REV 00 Sep 18/19 A320-25-1BQBRemove and Install the X-fixation Bracket in
the Correct Position on the RH Over-HeadStowage Compartment Housing Assembly Page 181
CONF 001
TYPICAL
VIEW LOOKING DOWN
AA
C
HOUSING
(6)(7)
(2)
CLEARANCE2 mm
(0.079 in)
X-FIXATION BRACKETX-FIXATION BRACKET
BIN
HOUSING
FWD
ICN-A320-A-25XX1BQB-A-FAPE3-01DMV-A-001-01
A318/A319/A320/A321SERVICE BULLETIN
REV 00 Sep 18/19 A320-25-1BQBPage 182
CONF 002(12) Task A320-A-25-XX-1BQB-12002-600A-A - Remove and Install the X-Fixation
Bracket in the Correct Position on the RH OHSC Housing AssemblyJob Set-Up Information
Working Area
Impacted Zone Access / Work Location230 Work location From Frame 21 to Frame 35.8240 Work location From Frame 35.8 to Frame 47250 Work location From Frame 47 to Frame 64260 Work location From Frame 64 to Frame 66
Manpower/Resources/Skills
Man-hours 0.25 hMinimum Number of person 1Elapsed Time 0.25 hSkills Cabin
Referenced Information
Manuals/Drawings References/Sheets
AMM06-20-00, Page Block 00106-31-53, Page Block 001Task 20-21-11-911-001Task 25-24-41-400-802
Procedure(a) Standard Practices
1 For the identification of zones, refer to Ref. AMM 06-20-00, Page Block 001.2 For the Frame (FR) identification, refer to Ref. AMM 06-31-53, Page Block
001.3 Tag all the parts you must remove and retain to make the subsequent
installation easier.4 Put all the retained hardware in identified plastic bags and attach the bags
to the related unit.5 To torque tighten the standard threaded fasteners, refer to Ref. AMM Task
20-21-11-911-001.(b) Remove and install the x-fixation bracket in the correct position on the RH OHSC
housing.Refer to Ref. Fig. Remove and Install the X-fixation Bracket in the Correct Positionon the RH Over-Head Stowage Compartment Housing Assembly1 Remove:
Refer to Ref. Fig. Remove and Install the X-fixation Bracket in the CorrectPosition on the RH Over-Head Stowage Compartment Housing Assembly
4 SCREW Item (6) Retain
4 WASHER Item (7) Retain
1 BRACKET Item (2) Retain
A318/A319/A320/A321SERVICE BULLETIN
REV 00 Sep 18/19 A320-25-1BQBPage 183
2 Install:Refer to Ref. Fig. Remove and Install the X-fixation Bracket in the CorrectPosition on the RH Over-Head Stowage Compartment Housing Assembly
1 BRACKET Item (2) Retainedwith
4 WASHER Item (7) Retained
4 SCREW Item (6) Retained3 Make sure that the bracket item (2) is installed in ‘Flight Direction’ on the
housing, in front of the bracket of the bin assembly, to face each other,refer to Ref. Fig. Remove and Install the X-fixation Bracket in the CorrectPosition on the RH Over-Head Stowage Compartment Housing Assembly.
4 Torque the screws item (6) to 2.50 Nm (22.126 lbf.in.).5 Install the bin on the RH OHSC, refer to Ref. AMM Task 25-24-41-400-802.
A318/A319/A320/A321SERVICE BULLETIN
Figure ICN-A320-A-25XX1BQB-A-FAPE3-01DMS-A-002-01 SHEET 1/2REV 00 Sep 18/19 A320-25-1BQBRemove and Install the X-fixation Bracket in
the Correct Position on the RH Over-HeadStowage Compartment Housing Assembly Page 184
CONF 002
ATYPICAL
VIEW LOOKING AFT
B
VIEW SHOWN WITHOUT BINSTYPICAL
HOUSING
C
C
B
A
- Z230 Z260
A
A
A
A
ICN-A320-A-25XX1BQB-A-FAPE3-01DMS-A-002-01
A318/A319/A320/A321SERVICE BULLETIN
Figure ICN-A320-A-25XX1BQB-A-FAPE3-01DMT-A-001-01 SHEET 2/2REV 00 Sep 18/19 A320-25-1BQBRemove and Install the X-fixation Bracket in
the Correct Position on the RH Over-HeadStowage Compartment Housing Assembly Page 185
CONF 002
TYPICAL
VIEW LOOKING DOWN
AA
C
HOUSING
(6)(7)
(2)
CLEARANCE2 mm
(0.079 in)
X-FIXATION BRACKETX-FIXATION BRACKET
BIN
HOUSING
FWD
ICN-A320-A-25XX1BQB-A-FAPE3-01DMT-A-001-01
A318/A319/A320/A321SERVICE BULLETIN
REV 00 Sep 18/19 A320-25-1BQBPage 186
CONF 001(13) Task A320-A-25-XX-1BQB-13001-600A-A - Remove and Install the X-Fixation
Bracket in the Correct Position on the Special LH OHSC Bin AssemblyJob Set-Up Information
Working Area
Impacted Zone Access / Work Location250 Work location From Frame 63 to Frame 64260 Work location From Frame 64 to Frame 66
Manpower/Resources/Skills
Man-hours 0.25 hMinimum Number of person 1Elapsed Time 0.25 hSkills Cabin
Referenced Information
Manuals/Drawings References/Sheets
AMM06-20-00, Page Block 00106-31-53, Page Block 001Task 20-21-11-911-001Task 25-24-41-000-802
Procedure(a) Standard Practices
1 For the identification of zones, refer to Ref. AMM 06-20-00, Page Block 001.2 For the Frame (FR) identification, refer to Ref. AMM 06-31-53, Page Block
001.3 Tag all the parts you must remove and retain to make the subsequent
installation easier.4 Put all the retained hardware in identified plastic bags and attach the bags
to the related unit.5 To torque tighten the standard threaded fasteners, refer to Ref. AMM Task
20-21-11-911-001.(b) Remove and install the x-fixation bracket in the correct position on the LH OHSC
bin assembly.Refer to Ref. Fig. Remove and Install the X-fixation Bracket in the Correct Positionon the Special LH Over-Head Stowage Compartment Bin Assembly1 Remove the bin from the LH OHSC, refer to Ref. AMM Task
25-24-41-000-802.2 Remove:
Refer to Ref. Fig. Remove and Install the X-fixation Bracket in the CorrectPosition on the Special LH Over-Head Stowage Compartment Bin Assembly
4 SCREW Item (8) Retain
4 WASHER Item (7) Retain
1 BRACKET Item (3) Retain
A318/A319/A320/A321SERVICE BULLETIN
REV 00 Sep 18/19 A320-25-1BQBPage 187
3 Install:Refer to Ref. Fig. Remove and Install the X-fixation Bracket in the CorrectPosition on the Special LH Over-Head Stowage Compartment Bin Assembly
1 BRACKET Item (3) Retainedwith
4 WASHER Item (7) Retained
4 SCREW Item (8) Retained4 Make sure that the bracket item (3) is installed in ‘Flight Direction’ on the
bin assembly, aft of the bracket of the housing, to face each other, refer toRef. Fig. Remove and Install the X-fixation Bracket in the Correct Position onthe Special LH Over-Head Stowage Compartment Bin Assembly.
5 Torque the screws item (8) to 2.50 Nm (22.126 lbf.in.).
A318/A319/A320/A321SERVICE BULLETIN
Figure ICN-A320-A-25XX1BQB-A-FAPE3-00YPC-A-003-01 SHEET 1/2REV 00 Sep 18/19 A320-25-1BQBRemove and Install the X-fixation Bracket in
the Correct Position on the Special LH Over-Head Stowage Compartment Bin Assembly Page 188
CONF 001
A
A
TYPICALVIEW SHOWN WITHOUT HOUSING
B
A
A
BIN
- Z250 Z260
FR69
AFT PAX DOOR
FR66
FR63
B
C
ICN-A320-A-25XX1BQB-A-FAPE3-00YPC-A-003-01
A318/A319/A320/A321SERVICE BULLETIN
Figure ICN-A320-A-25XX1BQB-A-FAPE3-01DMW-A-001-01 SHEET 2/2REV 00 Sep 18/19 A320-25-1BQBRemove and Install the X-fixation Bracket in
the Correct Position on the Special LH Over-Head Stowage Compartment Bin Assembly Page 189
CONF 001
(8)(7)
(3)
C
BIN
AAFWD
VIEW LOOKING DOWN
X-FIXATION BRACKETX-FIXATION BRACKET
HOUSINGCLEARANCE
2 mm(0.079 in)
BIN
ICN-A320-A-25XX1BQB-A-FAPE3-01DMW-A-001-01
A318/A319/A320/A321SERVICE BULLETIN
REV 00 Sep 18/19 A320-25-1BQBPage 190
CONF 002(13) Task A320-A-25-XX-1BQB-13002-600A-A - Remove and Install the X-Fixation
Bracket in the Correct Position on the Special LH OHSC Bin AssemblyJob Set-Up Information
Working Area
Impacted Zone Access / Work Location250 Work location From Frame 63 to Frame 64260 Work location From Frame 64 to Frame 66
Manpower/Resources/Skills
Man-hours 0.25 hMinimum Number of person 1Elapsed Time 0.25 hSkills Cabin
Referenced Information
Manuals/Drawings References/Sheets
AMM06-20-00, Page Block 00106-31-53, Page Block 001Task 20-21-11-911-001Task 25-24-41-000-802
Procedure(a) Standard Practices
1 For the identification of zones, refer to Ref. AMM 06-20-00, Page Block 001.2 For the Frame (FR) identification, refer to Ref. AMM 06-31-53, Page Block
001.3 Tag all the parts you must remove and retain to make the subsequent
installation easier.4 Put all the retained hardware in identified plastic bags and attach the bags
to the related unit.5 To torque tighten the standard threaded fasteners, refer to Ref. AMM Task
20-21-11-911-001.(b) Remove and install the x-fixation bracket in the correct position on the LH OHSC
bin assembly.Refer to Ref. Fig. Remove and Install the X-fixation Bracket in the Correct Positionon the Special LH Over-Head Stowage Compartment Bin Assembly1 Remove the bin from the LH OHSC, refer to Ref. AMM Task
25-24-41-000-802.2 Remove:
Refer to Ref. Fig. Remove and Install the X-fixation Bracket in the CorrectPosition on the Special LH Over-Head Stowage Compartment Bin Assembly
4 SCREW Item (8) Retain
4 WASHER Item (7) Retain
1 BRACKET Item (3) Retain
A318/A319/A320/A321SERVICE BULLETIN
REV 00 Sep 18/19 A320-25-1BQBPage 191
3 Install:Refer to Ref. Fig. Remove and Install the X-fixation Bracket in the CorrectPosition on the Special LH Over-Head Stowage Compartment Bin Assembly
1 BRACKET Item (3) Retainedwith
4 WASHER Item (7) Retained
4 SCREW Item (8) Retained4 Make sure that the bracket item (3) is installed in ‘Flight Direction’ on the
bin assembly, aft of the bracket of the housing, to face each other, refer toRef. Fig. Remove and Install the X-fixation Bracket in the Correct Position onthe Special LH Over-Head Stowage Compartment Bin Assembly.
5 Torque the screws item (8) to 2.50 Nm (22.126 lbf.in.).
A318/A319/A320/A321SERVICE BULLETIN
Figure ICN-A320-A-25XX1BQB-A-FAPE3-00YPH-A-003-01 SHEET 1/2REV 00 Sep 18/19 A320-25-1BQBRemove and Install the X-fixation Bracket in
the Correct Position on the Special LH Over-Head Stowage Compartment Bin Assembly Page 192
CONF 002
A
TYPICALVIEW SHOWN WITHOUT HOUSING
B
A
A
BIN
FR69
AFT PAX DOOR
FR66
FR63
B
A
- Z250 Z260
C
ICN-A320-A-25XX1BQB-A-FAPE3-00YPH-A-003-01
A318/A319/A320/A321SERVICE BULLETIN
Figure ICN-A320-A-25XX1BQB-A-FAPE3-01DMY-A-001-01 SHEET 2/2REV 00 Sep 18/19 A320-25-1BQBRemove and Install the X-fixation Bracket in
the Correct Position on the Special LH Over-Head Stowage Compartment Bin Assembly Page 193
CONF 002
AAFWD
VIEW LOOKING DOWN
C
(8)(7)
(3)
BIN
X-FIXATION BRACKETX-FIXATION BRACKET
HOUSINGCLEARANCE
2 mm(0.079 in)
BIN
ICN-A320-A-25XX1BQB-A-FAPE3-01DMY-A-001-01
A318/A319/A320/A321SERVICE BULLETIN
REV 00 Sep 18/19 A320-25-1BQBPage 194
CONF 001(14) Task A320-A-25-XX-1BQB-14001-600A-A - Remove and Install the X-Fixation
Bracket in the Correct Position on the Special RH OHSC Bin AssemblyJob Set-Up Information
Working Area
Impacted Zone Access / Work Location250 Work location From Frame 63 to Frame 64260 Work location From Frame 64 to Frame 66
Manpower/Resources/Skills
Man-hours 0.25 hMinimum Number of person 1Elapsed Time 0.25 hSkills Cabin
Referenced Information
Manuals/Drawings References/Sheets
AMM06-20-00, Page Block 00106-31-53, Page Block 001Task 20-21-11-911-001Task 25-24-41-000-802
Procedure(a) Standard Practices
1 For the identification of zones, refer to Ref. AMM 06-20-00, Page Block 001.2 For the Frame (FR) identification, refer to Ref. AMM 06-31-53, Page Block
001.3 Tag all the parts you must remove and retain to make the subsequent
installation easier.4 Put all the retained hardware in identified plastic bags and attach the bags
to the related unit.5 To torque tighten the standard threaded fasteners, refer to Ref. AMM Task
20-21-11-911-001.(b) Remove and install the x-fixation bracket in the correct position on the RH OHSC
bin assembly.Refer to Ref. Fig. Remove and Install the X-fixation Bracket in the Correct Positionon the Special RH Over-Head Stowage Compartment Bin Assembly1 Remove the bin from the RH OHSC, refer to Ref. AMM Task
25-24-41-000-802.2 Remove:
Refer to Ref. Fig. Remove and Install the X-fixation Bracket in the CorrectPosition on the Special RH Over-Head Stowage Compartment Bin Assembly
4 SCREW Item (8) Retain
4 WASHER Item (7) Retain
1 BRACKET Item (4) Retain
A318/A319/A320/A321SERVICE BULLETIN
REV 00 Sep 18/19 A320-25-1BQBPage 195
3 Install:Refer to Ref. Fig. Remove and Install the X-fixation Bracket in the CorrectPosition on the Special RH Over-Head Stowage Compartment Bin Assembly
1 BRACKET Item (4) Retainedwith
4 WASHER Item (7) Retained
4 SCREW Item (8) Retained4 Make sure that the bracket item (4) is installed in ‘Flight Direction’ on the
bin assembly, aft of the bracket of the housing, to face each other, refer toRef. Fig. Remove and Install the X-fixation Bracket in the Correct Position onthe Special RH Over-Head Stowage Compartment Bin Assembly.
5 Torque the screws item (8) to 2.50 Nm (22.126 lbf.in.).
A318/A319/A320/A321SERVICE BULLETIN
Figure ICN-A320-A-25XX1BQB-A-FAPE3-00YPE-A-003-01 SHEET 1/2REV 00 Sep 18/19 A320-25-1BQBRemove and Install the X-fixation Bracket in
the Correct Position on the Special RH Over-Head Stowage Compartment Bin Assembly Page 196
CONF 001
A
FR69
AFT PAX DOOR
FR66
FR63
B
TYPICALVIEW SHOWN WITHOUT HOUSING
B
A
A
BIN
A
- Z250 Z260
C
ICN-A320-A-25XX1BQB-A-FAPE3-00YPE-A-003-01
A318/A319/A320/A321SERVICE BULLETIN
Figure ICN-A320-A-25XX1BQB-A-FAPE3-01DMX-A-001-01 SHEET 2/2REV 00 Sep 18/19 A320-25-1BQBRemove and Install the X-fixation Bracket in
the Correct Position on the Special RH Over-Head Stowage Compartment Bin Assembly Page 197
CONF 001
C
AAVIEW LOOKING DOWN
(8)(7)
(4)
BIN
X-FIXATION BRACKETX-FIXATION BRACKET
HOUSINGCLEARANCE
2 mm(0.079 in)
BIN
FWD
ICN-A320-A-25XX1BQB-A-FAPE3-01DMX-A-001-01
A318/A319/A320/A321SERVICE BULLETIN
REV 00 Sep 18/19 A320-25-1BQBPage 198
(15) Task A320-A-25-XX-1BQB-15001-600A-A - Remove and Install the X-FixationBracket with Fixation Holder in the Correct Position on the LH OHSC HousingAssemblyJob Set-Up Information
Working Area
Impacted Zone Access / Work Location250 Work location From Frame 63 to Frame 64260 Work location From Frame 64 to Frame 66
Manpower/Resources/Skills
Man-hours 0.25 hMinimum Number of person 1Elapsed Time 0.25 hSkills Cabin
Referenced Information
Manuals/Drawings References/Sheets
AMM
06-20-00, Page Block 00106-31-53, Page Block 001Task 20-21-11-911-001Task 23-73-45-000-001Task 23-73-45-400-001Task 25-24-41-400-802Task 25-25-11-000-001Task 25-25-11-400-001
Procedure(a) Standard Practices
1 For the identification of zones, refer to Ref. AMM 06-20-00, Page Block 001.2 For the Frame (FR) identification, refer to Ref. AMM 06-31-53, Page Block
001.3 Tag all the parts you must remove and retain to make the subsequent
installation easier.4 Put all the retained hardware in identified plastic bags and attach the bags
to the related unit.5 To torque tighten the standard threaded fasteners, refer to Ref. AMM Task
20-21-11-911-001.(b) Remove and install the x-fixation bracket in the correct position on the LH OHSC
housing.Refer to Ref. Fig. Remove and Install the X-fixation Bracket with Holder in theCorrect Position on the LH Over-Head Stowage Compartment Housing Assembly1 Remove the PSU, refer to Ref. AMM Task 23-73-45-000-001.2 Remove the filler panels, as necessary, refer to Ref. AMM Task
25-25-11-000-001.
A318/A319/A320/A321SERVICE BULLETIN
REV 00 Sep 18/19 A320-25-1BQBPage 199
3 Remove:Refer to Ref. Fig. Remove and Install the X-fixation Bracket with Holder inthe Correct Position on the LH Over-Head Stowage Compartment HousingAssembly
4 NUT Item (10) Retain
4 WASHER Item (7) Retain
4 SCREW Item (9) Retain
1 BRACKET Item (1) Retain
1 HOLDER Item (11) Retain4 Install:
Refer to Ref. Fig. Remove and Install the X-fixation Bracket with Holder inthe Correct Position on the LH Over-Head Stowage Compartment HousingAssembly
1 BRACKET Item (1) Retained
1 HOLDER Item (11) Retainedwith
4 WASHER Item (7) Retained
4 SCREW Item (9) Retained
4 NUT Item (10) Retained5 Make sure that the bracket item (1) is installed in ‘Flight Direction’ on the
housing, in front of the bracket of the bin assembly, to face each other,refer to Ref. Fig. Remove and Install the X-fixation Bracket with Holder inthe Correct Position on the LH Over-Head Stowage Compartment HousingAssembly.
6 Torque the nuts item (10) to 2.50 Nm (22.126 lbf.in.).7 Install the bin on the LH OHSC, refer to Ref. AMM Task 25-24-41-400-802.8 Install the filler panels, if removed, refer to Ref. AMM Task
25-25-11-400-001.9 Install the PSU, refer to Ref. AMM Task 23-73-45-400-001.
A318/A319/A320/A321SERVICE BULLETIN
Figure ICN-A320-A-25XX1BQB-A-FAPE3-00YPK-A-002-01 SHEET 1/2REV 00 Sep 18/19 A320-25-1BQBRemove and Install the X-fixation Bracket with
Holder in the Correct Position on the LH Over-Head Stowage Compartment Housing Assembly Page 200
CONF 001
A
FR69
AFT PAX DOOR
FR66
FR63
B
FWD
VIEW LOOKING OUTBOARD
A A
HOUSING
VIEW SHOWN WITHOUT BIN
B
A
- Z250 Z260
C
ICN-A320-A-25XX1BQB-A-FAPE3-00YPK-A-002-01
A318/A319/A320/A321SERVICE BULLETIN
Figure ICN-A320-A-25XX1BQB-A-FAPE3-00YPL-A-003-01 SHEET 2/2REV 00 Sep 18/19 A320-25-1BQBRemove and Install the X-fixation Bracket with
Holder in the Correct Position on the LH Over-Head Stowage Compartment Housing Assembly Page 201
CONF 001
AAVIEW LOOKING DOWN
FWD
X-FIXATION BRACKETX-FIXATION BRACKET
BIN
HOUSING
CLEARANCE2 mm
(0.079 in)
C
(9)(7)
(10)
(1)
(11)
ICN-A320-A-25XX1BQB-A-FAPE3-00YPL-A-003-01
A318/A319/A320/A321SERVICE BULLETIN
REV 00 Sep 18/19 A320-25-1BQBPage 202
CONF 002(15) Task A320-A-25-XX-1BQB-15002-600A-A - Remove and Install the X-Fixation
Bracket with Fixation Holder in the Correct Position on the LH OHSC HousingAssemblyJob Set-Up Information
Working Area
Impacted Zone Access / Work Location250 Work location From Frame 63 to Frame 64260 Work location From Frame 64 to Frame 66
Manpower/Resources/Skills
Man-hours 0.25 hMinimum Number of person 1Elapsed Time 0.25 hSkills Cabin
Referenced Information
Manuals/Drawings References/Sheets
AMM
06-20-00, Page Block 00106-31-53, Page Block 001Task 20-21-11-911-001Task 23-73-45-000-001Task 23-73-45-400-001Task 25-24-41-400-802Task 25-25-11-000-001Task 25-25-11-400-001
Procedure(a) Standard Practices
1 For the identification of zones, refer to Ref. AMM 06-20-00, Page Block 001.2 For the Frame (FR) identification, refer to Ref. AMM 06-31-53, Page Block
001.3 Tag all the parts you must remove and retain to make the subsequent
installation easier.4 Put all the retained hardware in identified plastic bags and attach the bags
to the related unit.5 To torque tighten the standard threaded fasteners, refer to Ref. AMM Task
20-21-11-911-001.(b) Remove and install the x-fixation bracket in the correct position on the LH OHSC
housing.Refer to Ref. Fig. Remove and Install the X-fixation Bracket with Holder in theCorrect Position on the LH Over-Head Stowage Compartment Housing Assembly1 Remove the PSU, refer to Ref. AMM Task 23-73-45-000-001.2 Remove the filler panels, as necessary, refer to Ref. AMM Task
25-25-11-000-001.
A318/A319/A320/A321SERVICE BULLETIN
REV 00 Sep 18/19 A320-25-1BQBPage 203
3 Remove:Refer to Ref. Fig. Remove and Install the X-fixation Bracket with Holder inthe Correct Position on the LH Over-Head Stowage Compartment HousingAssembly
4 NUT Item (10) Retain
4 WASHER Item (7) Retain
4 SCREW Item (9) Retain
1 BRACKET Item (1) Retain
1 HOLDER Item (11) Retain4 Install:
Refer to Ref. Fig. Remove and Install the X-fixation Bracket with Holder inthe Correct Position on the LH Over-Head Stowage Compartment HousingAssembly
1 BRACKET Item (1) Retained
1 HOLDER Item (11) Retainedwith
4 WASHER Item (7) Retained
4 SCREW Item (9) Retained
4 NUT Item (10) Retained5 Make sure that the bracket item (1) is installed in ‘Flight Direction’ on the
housing, in front of the bracket of the bin assembly, to face each other,refer to Ref. Fig. Remove and Install the X-fixation Bracket with Holder inthe Correct Position on the LH Over-Head Stowage Compartment HousingAssembly.
6 Torque the nuts item (10) to 2.50 Nm (22.126 lbf.in.).7 Install the bin on the LH OHSC, refer to Ref. AMM Task 25-24-41-400-802.8 Install the filler panels, if removed, refer to Ref. AMM Task
25-25-11-400-001.9 Install the PSU, refer to Ref. AMM Task 23-73-45-400-001.
A318/A319/A320/A321SERVICE BULLETIN
Figure ICN-A320-A-25XX1BQB-A-FAPE3-00YPO-A-002-01 SHEET 1/2REV 00 Sep 18/19 A320-25-1BQBRemove and Install the X-fixation Bracket with
Holder in the Correct Position on the LH Over-Head Stowage Compartment Housing Assembly Page 204
CONF 002
FWD
VIEW LOOKING OUTBOARD
A A
HOUSING
VIEW SHOWN WITHOUT BIN
A
FR69
AFT PAX DOOR
FR66
FR63
B
A
- Z250 Z260
B
C
ICN-A320-A-25XX1BQB-A-FAPE3-00YPO-A-002-01
A318/A319/A320/A321SERVICE BULLETIN
Figure ICN-A320-A-25XX1BQB-A-FAPE3-00YPP-A-003-01 SHEET 2/2REV 00 Sep 18/19 A320-25-1BQBRemove and Install the X-fixation Bracket with
Holder in the Correct Position on the LH Over-Head Stowage Compartment Housing Assembly Page 205
CONF 002
AAVIEW LOOKING DOWN
FWD
X-FIXATION BRACKETX-FIXATION BRACKET
BIN
HOUSING
CLEARANCE2 mm
(0.079 in)
C
(9)(7)
(10)
(1)
(11)
ICN-A320-A-25XX1BQB-A-FAPE3-00YPP-A-003-01
A318/A319/A320/A321SERVICE BULLETIN
REV 00 Sep 18/19 A320-25-1BQBPage 206
CONF 001(16) Task A320-A-25-XX-1BQB-16001-600A-A - Remove and Install the X-Fixation
Bracket with Fixation Holder in the Correct Position on the RH OHSC HousingAssemblyJob Set-Up Information
Working Area
Impacted Zone Access / Work Location250 Work location From Frame 63 to Frame 64260 Work location From Frame 64 to Frame 66
Manpower/Resources/Skills
Man-hours 0.25 hMinimum Number of person 1Elapsed Time 0.25 hSkills Cabin
Referenced Information
Manuals/Drawings References/Sheets
AMM
06-20-00, Page Block 00106-31-53, Page Block 001Task 20-21-11-911-001Task 23-73-45-000-001Task 23-73-45-400-001Task 25-24-41-400-802Task 25-25-11-000-001Task 25-25-11-400-001
Procedure(a) Standard Practices
1 For the identification of zones, refer to Ref. AMM 06-20-00, Page Block 001.2 For the Frame (FR) identification, refer to Ref. AMM 06-31-53, Page Block
001.3 Tag all the parts you must remove and retain to make the subsequent
installation easier.4 Put all the retained hardware in identified plastic bags and attach the bags
to the related unit.5 To torque tighten the standard threaded fasteners, refer to Ref. AMM Task
20-21-11-911-001.(b) Remove and install the x-fixation bracket in the correct position on the RH OHSC
housing.Refer to Ref. Fig. Remove and Install the X-fixation Bracket with Holder in theCorrect Position on the RH Over-Head Stowage Compartment Housing Assembly1 Remove the PSU, refer to Ref. AMM Task 23-73-45-000-001.2 Remove the filler panels, as necessary, refer to Ref. AMM Task
25-25-11-000-001.
A318/A319/A320/A321SERVICE BULLETIN
REV 00 Sep 18/19 A320-25-1BQBPage 207
3 Remove:Refer to Ref. Fig. Remove and Install the X-fixation Bracket with Holder inthe Correct Position on the RH Over-Head Stowage Compartment HousingAssembly
4 NUT Item (10) Retain
4 WASHER Item (7) Retain
4 SCREW Item (9) Retain
1 BRACKET Item (2) Retain
1 HOLDER Item (11) Retain4 Install:
Refer to Ref. Fig. Remove and Install the X-fixation Bracket with Holder inthe Correct Position on the RH Over-Head Stowage Compartment HousingAssembly
1 BRACKET Item (2) Retained
1 HOLDER Item (11) Retainedwith
4 WASHER Item (7) Retained
4 SCREW Item (9) Retained
4 NUT Item (10) Retained5 Make sure that the bracket item (2) is installed in ‘Flight Direction’ on the
housing, in front of the bracket of the bin assembly, to face each other,refer to Ref. Fig. Remove and Install the X-fixation Bracket with Holder inthe Correct Position on the RH Over-Head Stowage Compartment HousingAssembly.
6 Torque the nuts item (10) to 2.50 Nm (22.126 lbf.in.).7 Install the bin on the RH OHSC, refer to Ref. AMM Task 25-24-41-400-802.8 Install the filler panels, if removed, refer to Ref. AMM Task
25-25-11-400-001.9 Install the PSU, refer to Ref. AMM Task 23-73-45-400-001.
A318/A319/A320/A321SERVICE BULLETIN
Figure ICN-A320-A-25XX1BQB-A-FAPE3-00YPM-A-003-01 SHEET 1/2REV 00 Sep 18/19 A320-25-1BQBRemove and Install the X-fixation Bracket with
Holder in the Correct Position on the RH Over-Head Stowage Compartment Housing Assembly Page 208
CONF 001
A
- Z250 Z260
A
FR69
AFT PAX DOOR
FR66
FR63
B
FWD
HOUSING
A A
VIEW LOOKING OUTBOARDVIEW SHOWN WITHOUT BIN
B
C
ICN-A320-A-25XX1BQB-A-FAPE3-00YPM-A-003-01
A318/A319/A320/A321SERVICE BULLETIN
Figure ICN-A320-A-25XX1BQB-A-FAPE3-00YPN-A-003-01 SHEET 2/2REV 00 Sep 18/19 A320-25-1BQBRemove and Install the X-fixation Bracket with
Holder in the Correct Position on the RH Over-Head Stowage Compartment Housing Assembly Page 209
CONF 001
AAVIEW LOOKING DOWN
C
X-FIXATION BRACKETX-FIXATION BRACKET
BIN
HOUSING
CLEARANCE2 mm
(0.079 in)
(9)(7)
(10)
(2)
(11)
FWD
ICN-A320-A-25XX1BQB-A-FAPE3-00YPN-A-003-01
A318/A319/A320/A321SERVICE BULLETIN
REV 00 Sep 18/19 A320-25-1BQBPage 210
CONF ALLD. PREPARATION FOR TEST
NoneE. TEST
CONF 001(1) Task A320-A-25-XX-1BQB-03001-340A-A - Testing
Job Set-Up InformationWorking Area
Impacted Zone Access / Work Location230 Work location From Frame 21 to Frame 35240 Work location From Frame 35 to Frame 47250 Work location From Frame 47 to Frame 64260 Work location From Frame 64 to Frame 66
Manpower/Resources/Skills
Man-hours 0.50 hMinimum Number of person 1Elapsed Time 0.50 hSkills Cabin
Referenced Information
Manuals/Drawings References/SheetsAMM Task 25-24-00-710-002
Procedure(a) If necessary, do the adjustment of the OHSC bin assembly, refer to Ref. AMM
Task 25-24-00-710-002.CONF 002
(1) Task A320-A-25-XX-1BQB-03002-340A-A - TestingJob Set-Up Information
Working Area
Impacted Zone Access / Work Location230 Work location From Frame 21 to Frame 35.8240 Work location From Frame 35.8 to Frame 47250 Work location From Frame 47 to Frame 64260 Work location From Frame 64 to Frame 66
Manpower/Resources/Skills
Man-hours 0.50 hMinimum Number of person 1Elapsed Time 0.50 hSkills Cabin
A318/A319/A320/A321SERVICE BULLETIN
REV 00 Sep 18/19 A320-25-1BQBPage 211
Referenced Information
Manuals/Drawings References/SheetsAMM Task 25-24-00-710-002
Procedure(a) If necessary, do the adjustment of the OHSC bin assembly, refer to Ref. AMM
Task 25-24-00-710-002.CONF ALL
F. CLOSE-UPCONF 001
(1) Task A320-A-25-XX-1BQB-04001-740A-A - Close-upJob Set-Up Information
Manpower/Resources/Skills
Man-hours 9.00 hMinimum Number of person 3Elapsed Time 3.00 h
Referenced Information
Manuals/Drawings References/SheetsAMM Task 25-24-41-400-802
Procedure(a) Make sure that the work areas are clean and clear of tools and other items of
equipment.(b) Do the close-up procedure as specified in the installation of the bin, refer to Ref.
AMM Task 25-24-41-400-802.(c) Put the aircraft back to its initial configuration.
CONF 002(1) Task A320-A-25-XX-1BQB-04002-740A-A - Close-up
Job Set-Up InformationManpower/Resources/Skills
Man-hours 12.00 hMinimum Number of person 3Elapsed Time 4.00 h
Referenced Information
Manuals/Drawings References/SheetsAMM Task 25-24-41-400-802
Procedure(a) Make sure that the work areas are clean and clear of tools and other items of
equipment.(b) Do the close-up procedure as specified in the installation of the bin, refer to Ref.
AMM Task 25-24-41-400-802.
A318/A319/A320/A321SERVICE BULLETIN
REV 00 Sep 18/19 A320-25-1BQBPage 212
(c) Put the aircraft back to its initial configuration.CONF ALL
G. ADMINISTRATIVE(1) Task A320-A-25-XX-1BQB-03001-90AA-A - Administrative
ProcedureConfirm in the applicable aircraft records that you have completed all the work definedin this Service Bulletin task set as required.
A318/A319/A320/A321SERVICE BULLETIN
APPENDIX
REV 00 Sep 18/19 A320-25-1BQBPage 213
APPENDIXA. 01 - Manpower Gantt Chart
01 - Manpower Gantt ChartFor an explanation of the man-hours and elapsed time, refer to the next page(s).
A318/A319/A320/A321SERVICE BULLETIN
APPENDIX
Figure ICN-A320-A-25XX1BQB-A-FAPE3-01DN3-A-001-01 SHEET 1/1REV 00 Sep 18/19 A320-25-1BQBManpower Gantt Chart - Inspection
without using Endoscope Camera Page 214
CONF 001
GET ACCESS
DO AN SDI OF THEX-FIXATION BRACKETS ONTHE LH OHSC WITHOUTUSING ENDOSCOPE CAMERA
TEST
CLOSE-UP
9.00 3.003
ELAPSED TIME ASSUMPTIONS SERVICE BULLETIN No A320-25-1BQB
MH ET/S
TOTAL MANHOURSSB ELAPSED TIME
21.509.50
STEPS
0
1.50 1.50
0.50 0.501
9.00 3.003
MH
ET/S:PER
MANHOURS
ELAPSED TIME PER STEPNUMBER OF PERSONS
01
02
THIS CHART IS ONLY A PROPOSAL.OPERATORS MAY DETERMINE THAT ANOTHER WAYTO DO THE WORK IS MORE SUITABLE FOR THEM.
IF A VSB IS INVOLVED, THE ASSOCIATED MANHOURSARE NOT REFLECTED IN THIS GANTT CHART.
01
02
NOTE:
PER
1
::
SB ELAPSED TIME(HOURS)
1 2 3 4 5 6 7 8 9
DO AN SDI OF THEX-FIXATION BRACKETS ONTHE RH OHSC WITHOUTUSING ENDOSCOPE CAMERA
1.50 1.501
ICN-A320-A-25XX1BQB-A-FAPE3-01DN3-A-001-01
A318/A319/A320/A321SERVICE BULLETIN
APPENDIX
Figure ICN-A320-A-25XX1BQB-A-FAPE3-01DN2-A-001-01 SHEET 1/1REV 00 Sep 18/19 A320-25-1BQBManpower Gantt Chart - Inspection
without using Endoscope Camera Page 215
CONF 002
GET ACCESS
DO AN SDI OF THEX-FIXATION BRACKETS ONTHE LH OHSC WITHOUTUSING ENDOSCOPE CAMERA
TEST
CLOSE-UP
12.00 4.003
ELAPSED TIME ASSUMPTIONS SERVICE BULLETIN No A320-25-1BQB
MH ET/S
TOTAL MANHOURSSB ELAPSED TIME
28.5012.50
STEPS
0
2.00 2.00
0.50 0.501
12.00 4.003
MH
ET/S:PER
MANHOURS
ELAPSED TIME PER STEPNUMBER OF PERSONS
01
02
THIS CHART IS ONLY A PROPOSAL.OPERATORS MAY DETERMINE THAT ANOTHER WAYTO DO THE WORK IS MORE SUITABLE FOR THEM.
IF A VSB IS INVOLVED, THE ASSOCIATED MANHOURSARE NOT REFLECTED IN THIS GANTT CHART.
01
02
NOTE:
PER
1
::
SB ELAPSED TIME(HOURS)
1 2 3 4 5 8 9 10 11
DO AN SDI OF THEX-FIXATION BRACKETS ONTHE RH OHSC WITHOUTUSING ENDOSCOPE CAMERA
6 7 12
2.00 2.001
ICN-A320-A-25XX1BQB-A-FAPE3-01DN2-A-001-01
A318/A319/A320/A321SERVICE BULLETIN
APPENDIX
Figure ICN-A320-A-25XX1BQB-A-FAPE3-01DN4-A-001-01 SHEET 1/2REV 00 Sep 18/19 A320-25-1BQBManpower Gantt Chart - Repair (Depending on the Inspection Result)
Page 216
CONF 001
ELAPSED TIME ASSUMPTION SERVICE BULLETIN No A320-25-1BQB
SB ELAPSED TIME(HOURS)
MH ET/S
TOTAL MANHOURSSB ELAPSED TIME
22.5010.50
STEPS
0.25 0.251
MH
ET/S:PER
MANHOURS
ELAPSED TIME PER STEPNUMBER OF PERSONS
01
02
THIS CHART IS ONLY A PROPOSAL.OPERATORS MAY DETERMINE THAT ANOTHER WAYTO DO THE WORK IS MORE SUITABLE FOR THEM.
01
02
NOTE:
PER
::
IF A VSB IS INVOLVED, THE ASSOCIATED MANHOURSARE NOT REFLECTED IN THIS GANTT CHART.
0.25 0.251
0.25 0.251
0.25 0.251
GET ACCESS 9.00 3.003
0.25 0.251
0.25 0.251
0.25 0.251
0.25 0.251
0.25 0.251
0 4 4.5 5
INSTALL THE MISSING X-FIXATION BRACKET ON THE LHOHSC BIN ASSEMBLY
INSTALL THE MISSING X-FIXATION BRACKET ON THE RHOHSC BIN ASSEMBLY
INSTALL THE MISSING X-FIXATION BRACKET ON THE LHOHSC HOUSING ASSEMBLY
INSTALL THE MISSING X-FIXATION BRACKET ON THE RHOHSC HOUSING ASSEMBLY
INSTALL THE MISSING X-FIXATION BRACKET ON THESPECIAL LH OHSC BIN ASSEMBLY
INSTALL THE MISSING X-FIXATION BRACKET ON THESPECIAL RH OHSC BIN ASSEMBLY
INSTALL THE MISSING X-FIXATION BRACKET WITH FIXATIONHOLDER ON THE LH OHSC HOUSING ASSEMBLY
INSTALL THE MISSING X-FIXATION BRACKET WITH FIXATIONHOLDER ON THE RH OHSC HOUSING ASSEMBLY
REMOVE AND INSTALL THE X-FIXATION BRACKET IN THECORRECT POSITION ON THE LH OHSC BIN ASSEMBLY
3 3.52 2.51 1.50.5
ICN-A320-A-25XX1BQB-A-FAPE3-01DN4-A-001-01
A318/A319/A320/A321SERVICE BULLETIN
APPENDIX
Figure ICN-A320-A-25XX1BQB-A-FAPE3-01DN5-A-001-01 SHEET 2/2REV 00 Sep 18/19 A320-25-1BQBManpower Gantt Chart - Repair (Depending on the Inspection Result)
Page 217
CONF 001
ELAPSED TIME ASSUMPTION SERVICE BULLETIN No A320-25-1BQB
SB ELAPSED TIME(HOURS)
MH ET/S
TOTAL MANHOURSSB ELAPSED TIME
22.5010.50
STEPS
0.50 0.501
MH
ET/S:PER
MANHOURS
ELAPSED TIME PER STEPNUMBER OF PERSONS
01
02
THIS CHART IS ONLY A PROPOSAL.OPERATORS MAY DETERMINE THAT ANOTHER WAYTO DO THE WORK IS MORE SUITABLE FOR THEM.
01
02
NOTE:
PER
::
IF A VSB IS INVOLVED, THE ASSOCIATED MANHOURSARE NOT REFLECTED IN THIS GANTT CHART.
0.25 0.251
0.25 0.251
0.25 0.251
0.25 0.251
0.25 0.251
0.25 0.251
0.25 0.251
9.00 3.003
9 9.5 108 8.57 7.56 6.55.5
TEST
CLOSE-UP
10.5
REMOVE AND INSTALL THE X-FIXATION BRACKET IN THECORRECT POSITION ON THE RH OHSC BIN ASSEMBLY
REMOVE AND INSTALL THE X-FIXATION BRACKET IN THECORRECT POSITION ON THE LH OHSC HOUSINGASSEMBLY
REMOVE AND INSTALL THE X-FIXATION BRACKET IN THECORRECT POSITION ON THE RH OHSC HOUSINGASSEMBLY
REMOVE AND INSTALL THE X-FIXATION BRACKET IN THECORRECT POSITION ON THE SPECIAL LH OHSCBIN ASSEMBLY
REMOVE AND INSTALL THE X-FIXATION BRACKET IN THECORRECT POSITION ON THE SPECIAL RH OHSCBIN ASSEMBLY
REMOVE AND INSTALL THE X-FIXATION BRACKET WITHFIXATION HOLDER IN THE CORRECT POSITION ON THELH OHSC HOUSING ASSEMBLY
REMOVE AND INSTALL THE X-FIXATION BRACKET WITHFIXATION HOLDER IN THE CORRECT POSITION ON THERH OHSC HOUSING ASSEMBLY
ICN-A320-A-25XX1BQB-A-FAPE3-01DN5-A-001-01
A318/A319/A320/A321SERVICE BULLETIN
APPENDIX
Figure ICN-A320-A-25XX1BQB-A-FAPE3-01DN6-A-001-01 SHEET 1/2REV 00 Sep 18/19 A320-25-1BQBManpower Gantt Chart - Repair (Depending on the Inspection Result)
Page 218
CONF 002
ELAPSED TIME ASSUMPTION SERVICE BULLETIN No A320-25-1BQB
SB ELAPSED TIME(HOURS)
MH ET/S
TOTAL MANHOURSSB ELAPSED TIME
27.5011.50
STEPS
0.25 0.251INSTALL THE MISSING X-FIXATION BRACKET WITH FIXATIONHOLDER ON THE LH OHSC HOUSING ASSEMBLY
MH
ET/S:PER
MANHOURS
ELAPSED TIME PER STEPNUMBER OF PERSONS
01
02
THIS CHART IS ONLY A PROPOSAL.OPERATORS MAY DETERMINE THAT ANOTHER WAYTO DO THE WORK IS MORE SUITABLE FOR THEM.
01
02
NOTE:
PER
::
IF A VSB IS INVOLVED, THE ASSOCIATED MANHOURSARE NOT REFLECTED IN THIS GANTT CHART.
0.25 0.251INSTALL THE MISSING X-FIXATION BRACKET ON THE LHOHSC BIN ASSEMBLY
0.25 0.251INSTALL THE MISSING X-FIXATION BRACKET ON THE RHOHSC BIN ASSEMBLY
GET ACCESS 12.00 4.003
0.25 0.251INSTALL THE MISSING X-FIXATION BRACKET ON THE LHOHSC HOUSING ASSEMBLY
0.25 0.251INSTALL THE MISSING X-FIXATION BRACKET ON THESPECIAL LH OHSC BIN ASSEMBLY
0.25 0.251INSTALL THE MISSING X-FIXATION BRACKET ON THE RHOHSC HOUSING ASSEMBLY
0.25 0.251REMOVE AND INSTALL THE X-FIXATION BRACKET IN THECORRECT POSITION ON THE LH OHSC BIN ASSEMBLY
0 4 5 5.54.53 3.52 2.51 1.50.5
ICN-A320-A-25XX1BQB-A-FAPE3-01DN6-A-001-01
A318/A319/A320/A321SERVICE BULLETIN
APPENDIX
Figure ICN-A320-A-25XX1BQB-A-FAPE3-01DN7-A-001-01 SHEET 2/2REV 00 Sep 18/19 A320-25-1BQBManpower Gantt Chart - Repair (Depending on the Inspection Result)
Page 219
CONF 002
ELAPSED TIME ASSUMPTION SERVICE BULLETIN No A320-25-1BQB
SB ELAPSED TIME(HOURS)
MH ET/S
TOTAL MANHOURSSB ELAPSED TIME
27.5011.50
STEPS
0.50 0.501TEST
MH
ET/S:PER
MANHOURS
ELAPSED TIME PER STEPNUMBER OF PERSONS
01
02
THIS CHART IS ONLY A PROPOSAL.OPERATORS MAY DETERMINE THAT ANOTHER WAYTO DO THE WORK IS MORE SUITABLE FOR THEM.
01
02
NOTE:
PER
::
IF A VSB IS INVOLVED, THE ASSOCIATED MANHOURSARE NOT REFLECTED IN THIS GANTT CHART.
0.25 0.251REMOVE AND INSTALL THE X-FIXATION BRACKET IN THECORRECT POSITION ON THE LH OHSC HOUSINGASSEMBLY
0.25 0.251REMOVE AND INSTALL THE X-FIXATION BRACKET IN THECORRECT POSITION ON THE RH OHSC BIN ASSEMBLY
0.25 0.251REMOVE AND INSTALL THE X-FIXATION BRACKET IN THECORRECT POSITION ON THE RH OHSC HOUSINGASSEMBLY
0.25 0.251REMOVE AND INSTALL THE X-FIXATION BRACKET IN THECORRECT POSITION ON THE SPECIAL LH OHSCBIN ASSEMBLY
0.25 0.251REMOVE AND INSTALL THE X-FIXATION BRACKET WITHFIXATION HOLDER IN THE CORRECT POSITION ON THELH OHSC HOUSING ASSEMBLY
12.00 4.003CLOSE-UP
9 10 10.59.58 8.57 7.56 6.5 11 11.5
ICN-A320-A-25XX1BQB-A-FAPE3-01DN7-A-001-01
A318/A319/A320/A321SERVICE BULLETIN
APPENDIX
REV 00 Sep 18/19 A320-25-1BQBPage 220
CONF ALLB. REPORTING SHEET
TITLE: EQUIPMENT/FURNISHINGS - OVERHEAD STOWAGE COMPARTMENTS -INSPECTION OF OHSC X-FIXATION BRACKETS
MODIFICATION No.: None
(1) SB Reporting statusThis Service Bulletin will only be incorporated into affected customized Maintenanceand Flight Operations Products if it is duly reported to Airbus.
(2) GENERAL informationThe SB Reporting policy is published in ISI 00.00.00135. This document providesinformation regarding: the SB Reporting means and benefits, the update ofcustomized Maintenance Products and customized Flight Operations Products.If this Service Bulletin has an operational impact, refer to paragraph "Flight OperationsProducts" for further information on the update of affected Flight Operations Products.
(3) SB Reporting procedureStandard practice to report SB is to use the online reporting application onAirbusWorld.Refer to ISI 00.00.00179:
- For complete information on reporting means to Airbus, Question 2 "What arethe 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 Bulletins?"
NOTE: ISI 00.00.00179 covers all the frequently asked questions about SB Reporting.It is revised on a regular basis.
A318/A319/A320/A321SERVICE BULLETIN
APPENDIX
REV 00 Sep 18/19 A320-25-1BQBPage 221
C. QUALITY PERCEPTION FORMUse 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 totake corrective action to further improve the quality of our Service Bulletin.We thank you for the time you have taken in completing this form.
Quality rating of this SB 4 3 2 1Quality rating of the Accomplishment Instructions 4 3 2 1Quality rating of the Illustrations 4 3 2 1Is this SB easy to understand ? Y / N
NOTE: Please rate on a scale of 1 to 4, with 4 being the highest score
If you have difficulties in the accomplishment of this SB please quote below the area(s) andgive a short description of the issue.
Planning Material InstructionsX Applicability X Tooling X PreparationX Reason X List of Materials
Operator SuppliedX Mod/Inspection
X Manpower X Kit content X TestX References X Re-identification X Close-upX Publication X IllustrationsX Industry Support
Comments :
Operator : Date :Name/TitlePlease return this form to :AIRBUS2, ROND POINT EMILE DEWOITINE31700 BLAGNACFRANCEOr via your Resident Customer Support Office.