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BD500-530012
2023-09-13 Page 1
Service Bulletin Fuselage - General - Verification of Previous Aircraft Repairs and Damage for Load Loop Analysis on the A220-300 BD500-530012 Issue No. 001 Copyright © 2023 Airbus Canada Limited Partnership All rights reserved. No part of this work may be reproduced or copied in any form or by any means without written permission of Airbus Canada Limited Partnership.
The Airbus and A220 logos are registered trademarks of Airbus Canada Limited Partnership.
The information, technical data and the designs disclosed herein are the exclusive property of Airbus Canada Limited Partnership or contain proprietary rights of others and are not to be used or disclosed to others without the written consent of Airbus Canada Limited Partnership. The recipient of this document, by its retention and use, agrees to hold in confidence the technical data and designs contained herein. The foregoing shall not apply to persons having proprietary rights to such information, technical data or such designs to the extent that such rights exist.
Manufacturer:
Airbus Canada Limited Partnership Customer Services 13100 Henri-Fabre Blvd., Mirabel, Quebec Canada J7N 3C6
BD500-530012
Intentionally left blank
2023-09-13 Page 2
BD500-530012
2023-09-13 Page 1 Table of contents The listed documents are included in Issue 001, dated 2023-09-13, of this publication.
Document title Data module code Issue date Applicable to Fuselage - General - Verification of Previous Aircraft Repairs and Damage for Load Loop Analysis on the A220-300 - Service Bulletin BD500-A-J53-00-12-00AAA-930A-A 2023-09-13 55003-55191, 55193, 55195-55196, 55198-55202, 55205, 55209-55210, 55228, 55231, 55244, 55246-55248, 55250 Verification of Previous Aircraft Repairs and Damage for Load Loop Analysis on the A220-300 - Accomplishment instruction BD500-A-J53-00-12-01AAA-933A-A 2023-09-13 55003-55191, 55193, 55195-55196, 55198-55202, 55205, 55209-55210, 55228, 55231, 55244, 55246-55248, 55250 Appendix A - A220-300 Tailcone Missed Loop 3 Inspection Areas BD500-A-J53-00-12-01AAA-910B-A 2023-09-13 55003-55191, 55193, 55195-55196, 55198-55202, 55205, 55209-55210, 55228, 55231, 55244, 55246-55248, 55250 Appendix B - A220-300 VStab Missed Loop 3 Inspection Areas BD500-A-J53-00-12-02AAA-910B-A 2023-09-13 55003-55191, 55193, 55195-55196, 55198-55202, 55205, 55209-55210, 55228, 55231, 55244, 55246-55248, 55250
BD500-530012
2023-09-13 Page 2 Document title Data module code Issue date Applicable to Appendix C - A220-300 Wing Missed Loop 3 Inspection Areas BD500-A-J53-00-12-03AAA-910B-A 2023-09-13 55003-55191, 55193, 55195-55196, 55198-55202, 55205, 55209-55210, 55228, 55231, 55244, 55246-55248, 55250
BD500-530012
See applicability on the first page of the DM BD500-A-J53-00-12-00AAA-930A-A BD500-A-J53-00-12-00AAA-930A-A 2023-09-13 Page 1 Fuselage - General - Verification of Previous Aircraft Repairs and Damage for Load Loop Analysis on the A220-300 - Service Bulletin
Applicability: 55003-55191, 55193, 55195-55196, 55198-55202, 55205, 55209-55210, 55228, 55231, 55244, 55246-55248, 55250
Table of contents Page Fuselage - General - Verification of Previous Aircraft Repairs and Damage for Load Loop
Analysis on the A220-300 - Service Bulletin1
References1
Service Bulletin1
Common information1
1 Maintenance Publications5
2 Operational Publications5
List of tables Page
1 References1
References Table 1 References Data Module/Technical Publication Title BD500-A-J53-00-12-01AAA-933A-A Verification of Previous Aircraft Repairs and Damage for Load Loop Analysis on the A220-300 - Accomplishment instruction BD500-A-J53-00-12-01AAA-910B-A Appendix A - A220-300 Tailcone Missed Loop 3 Inspection Areas BD500-A-J53-00-12-02AAA-910B-A Appendix B - A220-300 VStab Missed Loop 3 Inspection Areas BD500-A-J53-00-12-03AAA-910B-A Appendix C - A220-300 Wing Missed Loop 3 Inspection Areas Service Bulletin Common information THIS SERVICE BULLETIN IS SENT TO EACH OPERATOR. IF THE OPERATOR HAS LEASED AIRCRAFT, SEND THE SERVICE BULLETIN TO THE LESSEE. IF THE OPERATOR
HAS SOLD AIRCRAFT OR TRANSFERRED SPARES IN THE LAST SIX MONTHS, SEND
THIS SERVICE BULLETIN TO THE NEW OWNER, UNLESS CONFIRMATION WAS
RECEIVED THAT AIRBUS HAS INCLUDED THE NEW OPERATOR ON THE DISTRIBUTION LIST.
BD500-530012
See applicability on the first page of the DM BD500-A-J53-00-12-00AAA-930A-A BD500-A-J53-00-12-00AAA-930A-A 2023-09-13 Page 2 Management information Compliance category: Recommended (Service bulletin recommended to be accomplished to prevent significant operational disruptions) Task category: Administrative Original issue date: 2023-09-13 Impact list Impact (Maintenance publications):
Refer to the Documentation affected section of the Planning Information section.
Accomplishment limits None Replacement service bulletin None Revision information Initial issue Summary Applicability BD-500-1A11, Aircraft 55003 thru 55191, 55193, 55195, 55196, 55198 thru 55202, 55205, 55209, 55210, 55228, 55231, 55244, 55246 thru 55248, and 55250 Reason In-service repairs in the tailcone, the Vertical Stabilizer (VStab) and the wing structural areas can cause negative margins for the load envelopes, which will make it necessary to get verification from Airbus.
Description The identification of the previous aircraft repairs and damage is done. When applicable, the previous aircraft repairs and damage are reported to Airbus for analysis.
Concurrent requirements None Manpower It will take an estimated 1.5 h to complete this service bulletin.
Note These estimates do not include the man-hours necessary to do an inspection of the structure.
Material information None
BD500-530012
See applicability on the first page of the DM BD500-A-J53-00-12-00AAA-930A-A BD500-A-J53-00-12-00AAA-930A-A 2023-09-13 Page 3 Planning information Applicability Aircraft affected:
AIRCRAFT MODEL SERVICE AIRCRAFT
SERIAL NUMBER
PRODUCTION AIRCRAFT SERIAL
NUMBERS BD-500-1A11 55003 thru 55191, 55193, 55195, 55196, 55198 thru 55202, 55205, 55209, 55210, 55228, 55231, 55244, 55246 thru 55248, and 55250 There is no production effectivity.
Note The instructions in this service bulletin are only applicable to the systems and parts installed at the time of delivery of the aircraft or as changed by Airbus Service Bulletins.
Before you do this service bulletin, examine all Supplemental Type Certificates (STCs), Supplemental Type Approvals (STAs), or equivalent action changes to make sure you can complete this service bulletin.
Reason Problem and effect In-service repairs in the tailcone, the Vertical Stabilizer (VStab) and the wing structural areas can cause negative margins for the load envelopes, which will make it necessary to get verification from Airbus.
Objective/Solution This service bulletin gives the instructions to do a verification/record check and, if necessary, an inspection of previous damage and/or repairs done after the aircraft received its Certificate of Airworthiness (CofA). When applicable, the previous aircraft repairs and damage are reported to Airbus for analysis and approved disposition if necessary.
Description The identification of the previous aircraft repairs and damage is done. When applicable, the previous aircraft repairs and damage are reported to Airbus for analysis.
Compliance Recommended Service Bulletin Airbus recommends that this service bulletin be done within 48 months from the release date of this service bulletin, unless otherwise directed by the airworthiness authority of the operator.
Note If it is not possible to complete all the instructions in this service bulletin because of the configuration of the aircraft, speak with a CRC representative at 1 866 A220 CRC (1-866-222-0272) or 1-450-476-7676 or e-mail at A220_crc@abc.airbus for analysis and to get approved instructions to complete this service bulletin.
BD500-530012
See applicability on the first page of the DM BD500-A-J53-00-12-00AAA-930A-A BD500-A-J53-00-12-00AAA-930A-A 2023-09-13 Page 4 Note This service bulletin does not affect Airworthiness Limitations Items (ALIs) or Damage Tolerance Inspections (DTIs).
Concurrent requirements None Approval The technical content of this service bulletin has been approved under the authority of the TC- CA Design Approval Organization No: DAO #19-Q-02.
Manpower The man-hours given below are estimates for direct labor done by an experienced crew on an aircraft prepared for maintenance.
These estimates do not include the time necessary for:
- Administrative functions such as planning, liaising, familiarization, and report writing.
- Non-productive elapsed time such as rest time, having meals, and crew shift changes.
- Elapsed time such as for paint to dry, sealant to cure, and fuel tank venting.
- Preparation for modification (unless specified in the Accomplishment Instructions) such as cleaning and getting parts, tools, consumables, and ground equipment.
- Quality assurance inspections, troubleshooting and/or correction of discrepancies found when a task is done.
- All other activities that are not considered by Airbus as directly related to the accomplishment of this procedure.
It will take an estimated 1.5 h to complete this service bulletin. The man-hours are divided as shown in the table that follows:
TASK MAN-HOURS Job Set-Up 0.0 h Procedure 1.5 h Test 0.0 h Job Close-Up 0.0 h Note These estimates do not include the man-hours necessary to do an inspection of the structure.
Weight and balance Not changed Electrical load data Not changed
BD500-530012
See applicability on the first page of the DM BD500-A-J53-00-12-00AAA-930A-A BD500-A-J53-00-12-00AAA-930A-A End of data module 2023-09-13 Page 5 Referenced documentation Refer to the SB Introduction document BD500-000000 for definition or explanation of service bulletin content.
For Airbus reference only: Restriction and/or Special Instruction RSI C-500-000-51-0014, Revision C For Airbus reference only: PCR 62592 Documentation affected 1 Maintenance Publications None 2 Operational Publications None Industry support information This Service Bulletin is part of an AIRBUS monitored retrofit campaign.
For the organization of this retrofit, contact your AIRBUS Customer Services Program Support Program Manager.
For aircraft under warranty and for aircraft out of warranty at the time of the initial issue date of this Service Bulletin:
AIRBUS will credit up to 1.5 man-hours at the agreed in-house warranty labor rate for claims received no later than 90 days after completion of the last affected aircraft of your fleet, for the accomplishment of this Service Bulletin within 48 months after the initial issue date of the Service Bulletin.
Material information None Accomplishment instructions BD500-A-J53-00-12-01AAA-933A-A Additional information Additional information Appendix A: Refer to BD500-A-J53-00-12-01AAA-910B-A Appendix B: Refer to BD500-A-J53-00-12-02AAA-910B-A Appendix C: Refer to BD500-A-J53-00-12-03AAA-910B-A
BD500-530012
Intentionally left blank See applicability on the first page of the DM BD500-A-J53-00-12-00AAA-930A-A BD500-A-J53-00-12-00AAA-930A-A 2023-09-13 Page 6
BD500-530012
See applicability on the first page of the DM BD500-A-J53-00-12-01AAA-933A-A BD500-A-J53-00-12-01AAA-933A-A 2023-09-13 Page 1 Verification of Previous Aircraft Repairs and Damage for Load Loop Analysis on the A220-300 - Accomplishment instruction
Applicability: 55003-55191, 55193, 55195-55196, 55198-55202, 55205, 55209-55210, 55228, 55231, 55244, 55246-55248, 55250
Table of contents Page Verification of Previous Aircraft Repairs and Damage for Load Loop Analysis on the
A220-300 - Accomplishment instruction1
References1
Preliminary requirements1
Procedure2
1 Procedure2
2 Administrative4
Requirements after job completion4
List of tables Page
1 References1
2 Required conditions1
3 Support equipment2
4 Consumables, materials, and expendables2
5 Spares2
6 Applicable ATA for Repair or Damages3
7 Required conditions4
References Table 1 References Data Module/Technical Publication Title BD500-A-J53-00-12-01AAA-910B-A Appendix A - A220-300 Tailcone Missed Loop 3 Inspection Areas BD500-A-J53-00-12-02AAA-910B-A Appendix B - A220-300 VStab Missed Loop 3 Inspection Areas BD500-A-J53-00-12-03AAA-910B-A Appendix C - A220-300 Wing Missed Loop 3 Inspection Areas Preliminary requirements Required conditions Table 2 Required conditions Action/Condition Data Module/Technical publication None
BD500-530012
See applicability on the first page of the DM BD500-A-J53-00-12-01AAA-933A-A BD500-A-J53-00-12-01AAA-933A-A 2023-09-13 Page 2 Support equipment Table 3 Support equipment Name Identification/Reference Quantity Remark None Consumables, materials, and expendables Table 4 Consumables, materials, and expendables Name Identification/Reference Quantity Remark None Spares Table 5 Spares Name Identification/Reference Quantity Remark None Safety conditions None Procedure 1 Procedure
1.1 If it is not possible to complete all the instructions in this service bulletin because of the configuration of the aircraft, speak with a CRC representative at 1 866 A220 CRC (1-866-222-0272) or 1-450-476-7676 or e-mail at A220_crc@abc.airbus for analysis and to get an approved disposition to complete this service bulletin.
1.2 Identify previous in-service repairs, damage and non-conformity as follows:
Note Speak with a CRC representative at 1 866 A220 CRC (1-866-222-0272) or 1-450-476-7676 or e-mail at A220_crc@abc.airbus for acceptance of the method used to do these steps.
Note If it is not possible to correctly identify pre-existing repairs and/or damage within ASRP-permitted damage limits from the aircraft maintenance