A318/A319/A320/A321 31700 BLAGNAC CONF ALL ATA SYSTEM…

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A318/A319/A320/A321 SERVICE BULLETIN REV 00 Sep 18/19 A320-25-1BQB Page 1 CONF ALL AIRBUS 2, ROND POINT EMILE DEWOITINE 31700 BLAGNAC FRANCE 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 information contained in it be disclosed to unauthorized persons. It must not be reproduced in whole or in part without permission in writing from the owners of the copyright. Requests for reproduction of any data in this document and the media authorized for it must be addressed to Airbus. ATA SYSTEM: 25 TITLE: EQUIPMENT/FURNISHINGS - OVERHEAD STOWAGE COMPARTMENTS - INSPECTION OF OHSC X-FIXATION BRACKETS MODIFICATION No.: None

Transcript of A318/A319/A320/A321 31700 BLAGNAC CONF ALL ATA SYSTEM…

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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

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ATA SYSTEM: 25

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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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

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Figure ICN-A320-A-25XX1BQB-A-FAPE3-00YPI-A-002-01 SHEET 1/1REV 00 Sep 18/19 A320-25-1BQBSummary

Page 7

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

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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

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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

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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.

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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

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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

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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

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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

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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

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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)

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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)

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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

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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.

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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

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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

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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

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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

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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

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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

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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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A318/A319/A320/A321SERVICE BULLETIN

REV 00 Sep 18/19 A320-25-1BQBPage 35

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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A318/A319/A320/A321SERVICE BULLETIN

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.

Page 37: A318/A319/A320/A321 31700 BLAGNAC CONF ALL ATA SYSTEM…

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

Page 38: A318/A319/A320/A321 31700 BLAGNAC CONF ALL ATA SYSTEM…

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

Page 39: A318/A319/A320/A321 31700 BLAGNAC CONF ALL ATA SYSTEM…

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

Page 40: A318/A319/A320/A321 31700 BLAGNAC CONF ALL ATA SYSTEM…

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

Page 41: A318/A319/A320/A321 31700 BLAGNAC CONF ALL ATA SYSTEM…

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

Page 42: A318/A319/A320/A321 31700 BLAGNAC CONF ALL ATA SYSTEM…

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

Page 43: A318/A319/A320/A321 31700 BLAGNAC CONF ALL ATA SYSTEM…

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

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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

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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.

Page 46: A318/A319/A320/A321 31700 BLAGNAC CONF ALL ATA SYSTEM…

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

Page 47: A318/A319/A320/A321 31700 BLAGNAC CONF ALL ATA SYSTEM…

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

Page 48: A318/A319/A320/A321 31700 BLAGNAC CONF ALL ATA SYSTEM…

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

Page 49: A318/A319/A320/A321 31700 BLAGNAC CONF ALL ATA SYSTEM…

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

Page 50: A318/A319/A320/A321 31700 BLAGNAC CONF ALL ATA SYSTEM…

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

Page 51: A318/A319/A320/A321 31700 BLAGNAC CONF ALL ATA SYSTEM…

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

Page 52: A318/A319/A320/A321 31700 BLAGNAC CONF ALL ATA SYSTEM…

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

Page 53: A318/A319/A320/A321 31700 BLAGNAC CONF ALL ATA SYSTEM…

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

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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.

Page 55: A318/A319/A320/A321 31700 BLAGNAC CONF ALL ATA SYSTEM…

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

Page 56: A318/A319/A320/A321 31700 BLAGNAC CONF ALL ATA SYSTEM…

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

Page 57: A318/A319/A320/A321 31700 BLAGNAC CONF ALL ATA SYSTEM…

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

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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

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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

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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

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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

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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.

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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

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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.

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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.

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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.

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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

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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

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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

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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

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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

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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.

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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.

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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

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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

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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

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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

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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

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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.

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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.

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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

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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

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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

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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

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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.

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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.

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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

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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

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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

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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

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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

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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

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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.

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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.

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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

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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.

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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.

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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.).

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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

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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

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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

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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.).

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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

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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

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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

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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.).

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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

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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

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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.

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(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.).

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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

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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

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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

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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.

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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

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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

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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

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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.

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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

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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

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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

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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.

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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

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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

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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.

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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.

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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

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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

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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

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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.).

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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

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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

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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

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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.).

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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

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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

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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

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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.).

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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

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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

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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.

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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.

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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

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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

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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.

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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.

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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

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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

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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.

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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.

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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

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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

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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

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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.).

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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

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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

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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

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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.).

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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

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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

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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

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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.).

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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

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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

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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

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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.).

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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

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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

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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

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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.

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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

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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

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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

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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.

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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

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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

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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

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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.

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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

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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

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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

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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.

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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

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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

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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

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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.).

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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

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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

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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

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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.).

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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

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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

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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

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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.).

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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

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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

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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.

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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.

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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

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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

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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.

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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.

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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

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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

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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.

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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.

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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

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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

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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

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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.

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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.

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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).

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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

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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

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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

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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

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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

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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

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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.

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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.