On this page
Copies · 2
Copies of this document that the FAA filed in AD dockets on regulations.gov, newest revision first. A newer revision may exist.
© Airbus S.A.S. Filed by the FAA in regulations.gov docket FAA-2025-0345, the docket of AD 2025-14-09. Not covered by OpenAirDocs’ CC0 dedication.
© Airbus S.A.S. Filed by the FAA in regulations.gov docket FAA-2022-1248, the docket of AD 2022-27-01. Not covered by OpenAirDocs’ CC0 dedication.
- Manufacturer
- Airbus
- Type
- Service Bulletin
- Number
- A350-57-P069
- Latest revision known
- A350-57-P069, Revision 1
- Copies
- 2 files of 2 revisions
A newer revision may exist than any OpenAirDocs knows of: check with the manufacturer.
Text · 286
Revision 1, the newest copy. From the PDF’s text layer: layout, tables and figures are lost. The PDF is the document. © Airbus S.A.S. Filed by the FAA in regulations.gov docket FAA-2025-0345, the docket of AD 2025-14-09. Not covered by OpenAirDocs’ CC0 dedication.
Query with SQL
duckdb -csv -c "SELECT p.page, p.text_source, p.text, f.rights_holder, f.license FROM 'https://openairdocs.org/data/latest/service_document_file_page.parquet' p JOIN 'https://openairdocs.org/data/latest/service_document_file.parquet' f USING (file_sha256) WHERE p.file_sha256 = '39e2d35d43fffb61abfaa9e53507250a80e9664abe034974cf302ced4aa5636e' ORDER BY p.page"
Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.
SELECT p.page, p.text_source, p.text, f.rights_holder, f.license FROM 'https://openairdocs.org/data/latest/service_document_file_page.parquet' p JOIN 'https://openairdocs.org/data/latest/service_document_file.parquet' f USING (file_sha256) WHERE p.file_sha256 = '39e2d35d43fffb61abfaa9e53507250a80e9664abe034974cf302ced4aa5636e' ORDER BY p.page
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
A350
SERVICE BULLETIN REV 00 Nov 16/21 A350-57-P069 REV 01 Jun 07/24 Page 1
CONF ALL AIRBUS 2, ROND POINT EMILE DEWOITINE 31700 BLAGNAC FRANCE
The content of this document is the property of Airbus. All rights including copyrights are reserved.
It is supplied in confidence and commercial security on its contents must be maintained.
It must not be used for any purpose other than that for which it is supplied, nor may information contained in it be disclosed to unauthorized persons.
It must not be reproduced in whole or in part without permission in writing from the owners of the copyright. Requests for reproduction of any data in this document and the media authorized for it must be addressed to Airbus.
MANDATORY MANDATORY MANDATORY ATA SYSTEM: 57 TITLE: WINGS - CENTER WING - FASTENERS REPLACEMENT IN THE CENTER
WING BOX AT THE REAR SPAR AND THE FRONT SPAR LOWER AREA MODIFICATION No.:
116374L27002 116559L27019 CONF 001 003 004 116810L27029
A350
SERVICE BULLETIN
REVISION TRANSMITTAL SHEET REV 00 Nov 16/21 A350-57-P069 REV 01 Jun 07/24 Page 2 ATA SYSTEM: 57 TITLE: WINGS - CENTER WING - FASTENERS REPLACEMENT IN THE CENTER
WING BOX AT THE REAR SPAR AND THE FRONT SPAR LOWER AREA
CONF ALL
REVISION TRANSMITTAL SHEET This page transmits Revision No. 01 of Service Bulletin No. A350-57-P069.
A. ADDITIONAL WORK No additional work is required by this revision.
B. REASON Revision No. 01 issued to:
- Update the applicability of this Service Bulletin to add MSN 0005
- Replace the bonding code "P1" with "_1B3M2" in Fig.BE Sol.AA, Sol.AC and Fig.BD Sol.AA, Sol.AC
- Added the electrical bonding test reference
- Update the toque value in the nut item(56), between 6.30 Nm (55.760 lbf.in) and 8.20 Nm (72.576 lbf.in)
- Add instructions to remove/install hydraulic bracket in case of clash
- Add a note to allow removal/installation of swaged pin in case of clash.
NOTE: This revision satisfies the requirements of the subsequent Repair and Design Approval Form (RDAF) issued for the related MSNs.
RDAF MSNs 81006239/103/2023 0088, 0102, 0110, 0125, 0141, 0161, 0215, 0229, 0241, 0266, 0332, 0346, 0350, 0356, 0368, 0372, 0382, 0399 and 0420 81006239/195/2023 0006, 0007, 0008, 0009, 0010, 0011, 0012, 0013, 0021, 0025, 0033, 0036, 0042, 0047, 0063, 0069, 0076, 0078, 0083, 0088, 0090, 0100, 0102, 0106, 0110, 0114, 0125, 0126, 0132, 0141, 0143, 0161, 0163, 0172, 0207, 0211, 0214, 0215, 0229, 0237, 0241, 0249, 0257, 0266, 0332, 0346, 0350, 0356, 0368, 0372, 0382, 0399 and 0420 81006239/202/2024 0416 and 0468 81050077/053/2024 0024, 0027, 0048, 0064, 0115, 0135, 0149, 0160, 0164, 0175, 0182, 0190, 0199, 0200, 0204, 0210, 0250, 0265, 0267, 0277, 0282, 0313, 0395 and 0404 81120465/092/2023 0129 81120465/113/2023 0015 81120465/161/2023 0150 81120465/172/2023 0173 81120465/201/2024 0192 81123546/013/2024 0044, 0050, 0095, 0111, 0123, 0130,0 0142, 0177, 0181, 0185, 0189 and 0201 81125187/008/2023 0091 81172648/022/2024 0326, 0340, 0362, 0374, 0386, 0402, 0432 and 0446
A350
SERVICE BULLETIN
REVISION TRANSMITTAL SHEET REV 00 Nov 16/21 A350-57-P069 REV 01 Jun 07/24 Page 3 RDAF MSNs 81362782/004/2024 0045 81382688/011/2024 0219 C. CHANGES CONF 001
PLANNING INFORMATION APPLICABILITY - Note updated to extend the production applicability
- MOD data of 116810L27029 updated from Service Bulletin only to series solution only.
COMPLIANCE Accomplishment Timescale Note is updated.
REFERENCES T ask set A350-A-57-XX-P069- 01000-93AA-A Replacement of the Fasteners on the Rear Spar and the Front Spar Reference added.
INDUSTRY SUPPORT INFORMATION Sentences added.
MATERIAL INFORMATION
LIST OF NEW PARTS Part kit 57P069A01R01 Cost value updated.
Part kit 57P069A04R04 Cost value updated.
Components for task set A350- A-57-XX-P069-01000-93AA-A Replacement of the Fasteners on the Rear Spar and the Front Spar
- Updated PN EN6115V4-8 quantity from 12 to 8
- Updated PN EN6115V6-14 quantity from 12 to 8
- Updated PN ASNA2531-4 quantity from 8 to 4
- Updated PN ASNA2531-6 quantity from 8 to 4.
ACCOMPLISHMENT INSTRUCTIONS T ask set A350-A-57-XX-P069-01000-93AA-A Replacement of the Fasteners on the Rear Spar and the Front Spar
PREPARATION A350-A-57-XX-P069- 01001-540A-A General Job Set-Up Caution added.
PROCEDURE A350-A-57-XX-P069- 01001-920A-A Replace the Fasteners on the Front Spar, LH Side
- Added sentence in Standard Practices for fastener hole diameters and drill data in composite and hybrid structure
- Caution added
- Updated the word area with outer CWB
- CML added
- MP reference added for electrical bonding step
- Steps added for the removal and installation of hydraulic bracket to gain access to bracket item (20)
A350
SERVICE BULLETIN
REVISION TRANSMITTAL SHEET REV 00 Nov 16/21 A350-57-P069 REV 01 Jun 07/24 Page 4
- Note added for removal/installationof swaged pin in case of clash.
Fig.BB Sol.AA Replacement of the fasteners on the Front Spar
- Updated to add views for the removal and installation of hydraulic bracket
- Note added to avoid clash between the fasteners during removal or installation of fasteners
- Updated Fastener table to remove PNs EN6115V4-8, EN6115V6-14, ASNA2531-4 and ASNA2531-6.
A350-A-57-XX-P069- 03001-920A-A Replace the Fasteners on the Rear Spar, LH Side
- Warning and cautions are added
- Added sentence in Standard Practices for fastener hole diameters and drill data in composite and hybrid structure
- Updated the word area with outer CWB
- Note updated for the torque value
- CML added
- MP reference added for electrical bonding step
- Wording updated for the procedure step.
Fig.BE Sol.AA Replacement of the Fasteners on the Rear Spar, LH Side Illustration is updated to replace the bonding code "P1" with "_1B3M2".
Fig.BI Sol.AA Removal/ Installation of the Fittings on the Rear Spar, LH Side
- Note updated for the torque value A350-A-57-XX-P069- 02001-920A-A Replace the Fasteners on the Front Spar, RH Side
- Added sentence in Standard Practices for fastener hole diameters and drill data in composite and hybrid structure
- Caution added
- Updated the word area with outer CWB
- CML added
- MP reference added for electrical bonding step
- Steps added for the removal and installation of hydraulic bracket to gain access to bracket item (20).
Fig.BB Sol.AA Replacement of the fasteners on the Front Spar
- Updated to add views for the removal and installation of hydraulic bracket
- Note added to avoid clash between the fasteners during removal or installation of fasteners
- Updated Fastener table to remove PNs EN6115V4-8, EN6115V6-14, ASNA2531-4 and ASNA2531-6.
A350-A-57-XX-P069- 04001-920A-A Replace the Fasteners on the Rear Spar, RH Side
- Warning and cautions are added
- Added sentence in Standard Practices for fastener hole diameters and drill data in composite and hybrid structure
- Updated the word area with outer CWB
- Note updated for the torque value
- CML added
A350
SERVICE BULLETIN
REVISION TRANSMITTAL SHEET REV 00 Nov 16/21 A350-57-P069 REV 01 Jun 07/24 Page 5
- MP reference added for electrical bonding step
- Wording updated for the procedure step.
Fig.BD Sol.AA Replacement of the Fasteners on the Rear Spar, RH Side Illustration is updated to replace the bonding code "P1" with "_1B3M2".
Fig.BH Sol.AA Removal/ Installation of the Fittings on the Rear Spar, RH Side
- Note updated for the torque value.
T ask A350-A-57-XX-P069-02001-900A-C On Bench, Ream the Fittings Fig.BJ Sol.AB Ream the Fittings Illustration is updated to add note CONF 002
PLANNING INFORMATION APPLICABILITY - Note updated to extend the production applicability
- MOD data of 116810L27029 updated from Service Bulletin only to series solution only.
COMPLIANCE Accomplishment Timescale Note is updated.
REFERENCES T ask set A350-A-57-XX-P069- 01000-93AA-A Replacement of the Fasteners on the Rear Spar and the Front Spar Reference added.
INDUSTRY SUPPORT INFORMATION Sentences added.
MATERIAL INFORMATION
LIST OF NEW PARTS Part kit 57P069A03R02 Cost value updated.
Part kit 57P069A05R02 Cost value updated
ACCOMPLISHMENT INSTRUCTIONS T ask set A350-A-57-XX-P069-01000-93AA-A Replacement of the Fasteners on the Rear Spar and the Front Spar
PROCEDURE T ask A350-A-57-XX-P069-01003-920A-A Replace the Fasteners on the Front Spar, LH Side Fig.BB Sol.AC Replacement of the fasteners on the Front Spar
- Updated to add views for the removal and installation of hydraulic bracket
- Note added to avoid clash between the fasteners during removal or installation of fasteners
- Updated Fastener table to remove PNs EN6115V4-8, EN6115V6-14, ASNA2531-4 and ASNA2531-6.
A350-A-57-XX-P069- 03003-920A-A Replace the Fasteners on the Rear Spar, LH Side
- Warning and cautions are added
- Added sentence in Standard Practices for fastener hole diameters and drill data in composite and hybrid structure
- Updated the word area with outer CWB
A350
SERVICE BULLETIN
REVISION TRANSMITTAL SHEET REV 00 Nov 16/21 A350-57-P069 REV 01 Jun 07/24 Page 6
- CML added
- MP reference added for electrical bonding step
- Wording updated for the procedure step
- Fitting (10) quantity is updated from 2 to 1.
Fig.BE Sol.AC Replacement of the Fasteners on the Rear Spar, LH Side Illustration is updated to replace the bonding code "P1" with "_1B3M2".
A350-A-57-XX-P069- 02003-920A-A Replace the Fasteners on the Front Spar, RH Side
- Added sentence in Standard Practices for fastener hole diameters and drill data in composite and hybrid structure
- Caution added
- Updated the word area with outer CWB
- CML added
- MP reference added for electrical bonding step
- MBN item (21) is deleted
- Stripping diameter updated from 22 mm to 24 mm
- Wording updated for the procedure step
- Steps added for the removal and installation of hydraulic bracket to gain access to bracket item (20).
Fig.BB Sol.AC Replacement of the fasteners on the Front Spar
- Updated to add views for the removal and installation of hydraulic bracket
- Note added to avoid clash between the fasteners during removal or installation of fasteners
- Updated Fastener table to remove PNs EN6115V4-8, EN6115V6-14, ASNA2531-4 and ASNA2531-6.
A350-A-57-XX-P069- 04003-920A-A Replace the Fasteners on the Rear Spar, RH Side
- Warning and cautions are added
- Added sentence in Standard Practices for fastener hole diameters and drill data in composite and hybrid structure
- Updated the word area with outer CWB
- CML added.
- MP reference added for electrical bonding step
- Item number updated
- Wording updated for the procedure step.
Fig.BD Sol.AC Replacement of the Fasteners on the Rear Spar, RH Side Illustration is updated to replace the bonding code "P1" with "_1B3M2".
T ask A350-A-57-XX-P069-02002-900A-C On Bench, Ream the Fittings Fig.BJ Sol.AA Ream the Fittings Illustration is updated to add note CONF 003
PLANNING INFORMATION APPLICABILITY - Note updated to extend the production applicability
A350
SERVICE BULLETIN
REVISION TRANSMITTAL SHEET REV 00 Nov 16/21 A350-57-P069 REV 01 Jun 07/24 Page 7
- MOD data of 116810L27029 updated from Service Bulletin only to series solution only.
COMPLIANCE Accomplishment Timescale Note is updated.
REFERENCES T ask set A350-A-57-XX-P069- 01000-93AA-A Replacement of the Fasteners on the Rear Spar and the Front Spar Reference added.
INDUSTRY SUPPORT INFORMATION Sentences added.
MATERIAL INFORMATION
LIST OF NEW PARTS Part kit 57P069A02R01 Cost value and lead times updated.
Part kit 57P069A04R04 Cost value updated.
Components for task set A350- A-57-XX-P069-01000-93AA-A Replacement of the Fasteners on the Rear Spar and the Front Spar
- Updated PN EN6115V4-8 quantity from 12 to 8
- Updated PN EN6115V6-14 quantity from 12 to 8
- Updated PN ASNA2531-4 quantity from 8 to 4
- Updated PN ASNA2531-6 quantity from 8 to 4.
ACCOMPLISHMENT INSTRUCTIONS T ask set A350-A-57-XX-P069-01000-93AA-A Replacement of the Fasteners on the Rear Spar and the Front Spar
PREPARATION A350-A-57-XX-P069- 01001-540A-A General Job Set-Up Caution added.
PROCEDURE A350-A-57-XX-P069- 01001-920A-A Replace the Fasteners on the Front Spar, LH Side
- Added sentence in Standard Practices for fastener hole diameters and drill data in composite and hybrid structure
- Caution added
- Updated the word area with outer CWB
- CML added
- MP reference added for electrical bonding step
- Steps added for the removal and installation of hydraulic bracket to gain access to bracket item (20)
- Note added for removal/installationof swaged pin in case of clash.
Fig.BB Sol.AA Replacement of the fasteners on the Front Spar
- Updated to add views for the removal and installation of hydraulic bracket
- Note added to avoid clash between the fasteners during removal or installation of fasteners
- Updated Fastener table to remove PNs EN6115V4-8, EN6115V6-14, ASNA2531-4 and ASNA2531-6.
A350-A-57-XX-P069- 03002-920A-A Replace
- Warning and cautions are added
A350
SERVICE BULLETIN
REVISION TRANSMITTAL SHEET REV 00 Nov 16/21 A350-57-P069 REV 01 Jun 07/24 Page 8 the Fasteners on the Rear Spar, LH Side
- Added sentence in Standard Practices for fastener hole diameters and drill data in composite and hybrid structure
- Updated the word area with outer CWB
- Note updated for the torque value
- CML added
- MP reference added for electrical bonding step
- Wording updated for the procedure step.
Fig.BE Sol.AB Replacement of the Fasteners on the Rear Spar, LH Side Illustration is updated to replace the bonding code "P1" with "_1B3M2".
Fig.BI Sol.AA Removal/ Installation of the Fittings on the Rear Spar, LH Side
- Note updated for the torque value A350-A-57-XX-P069- 02001-920A-A Replace the Fasteners on the Front Spar, RH Side
- Added sentence in Standard Practices for fastener hole diameters and drill data in composite and hybrid structure
- Caution added
- Updated the word area with outer CWB
- CML added
- MP reference added for electrical bonding step
- Steps added for the removal and installation of hydraulic bracket to gain access to bracket item (20).
Fig.BB Sol.AA Replacement of the fasteners on the Front Spar
- Updated to add views for the removal and installation of hydraulic bracket
- Note added to avoid clash between the fasteners during removal or installation of fasteners
- Updated Fastener table to remove PNs EN6115V4-8, EN6115V6-14, ASNA2531-4 and ASNA2531-6.
A350-A-57-XX-P069- 04002-920A-A Replace the Fasteners on the Rear Spar, RH Side
- Warning and cautions are added
- Added sentence in Standard Practices for fastener hole diameters and drill data in composite and hybrid structure
- Updated the word area with outer CWB
- Note updated for the torque value
- CML added
- MP reference added for electrical bonding step
- Wording updated for the procedure step.
Fig.BD Sol.AB Replacement of the Fasteners on the Rear Spar, RH Side Illustration is updated to replace the bonding code "P1" with "_1B3M2".
Fig.BH Sol.AA Removal/ Installation of the Fittings on the Rear Spar, RH Side
- Note updated for the torque value.
T ask A350-A-57-XX-P069-02001-900A-C On Bench, Ream the Fittings
A350
SERVICE BULLETIN
REVISION TRANSMITTAL SHEET REV 00 Nov 16/21 A350-57-P069 REV 01 Jun 07/24 Page 9 Fig.BJ Sol.AB Ream the Fittings Illustration is updated to add note CONF 004
PLANNING INFORMATION APPLICABILITY - Note updated to extend the production applicability
- MOD data of 116810L27029 updated from Service Bulletin only to series solution only.
COMPLIANCE Accomplishment Timescale Note is updated.
REFERENCES T ask set A350-A-57-XX-P069- 01000-93AA-A Replacement of the Fasteners on the Rear Spar and the Front Spar Reference added.
INDUSTRY SUPPORT INFORMATION Sentences added.
MATERIAL INFORMATION
LIST OF NEW PARTS Part kit 57P069A02R01 Cost value and lead times updated.
Part kit 57P069A04R04 Cost value updated.
Components for task set A350- A-57-XX-P069-01000-93AA-A Replacement of the Fasteners on the Rear Spar and the Front Spar
- Updated PN EN6115V4-8 quantity from 12 to 8
- Updated PN EN6115V6-14 quantity from 12 to 8
- Updated PN ASNA2531-4 quantity from 8 to 4
- Updated PN ASNA2531-6 quantity from 8 to 4.
ACCOMPLISHMENT INSTRUCTIONS T ask set A350-A-57-XX-P069-01000-93AA-A Replacement of the Fasteners on the Rear Spar and the Front Spar
PREPARATION A350-A-57-XX-P069- 01001-540A-A General Job Set-Up Caution added.
PROCEDURE A350-A-57-XX-P069- 01002-920A-A Replace the Fasteners on the Front Spar, LH Side
- Added sentence in Standard Practices for fastener hole diameters and drill data in composite and hybrid structure
- Caution added
- Updated the word area with outer CWB
- CML added
- MP reference added for electrical bonding step
- Steps added for the removal and installation of hydraulic bracket to gain access to bracket item (20)
- Note added for removal/installationof swaged pin in case of clash.
A350
SERVICE BULLETIN
REVISION TRANSMITTAL SHEET REV 00 Nov 16/21 A350-57-P069 REV 01 Jun 07/24 Page 10 Fig.BB Sol.AB Replacement of the fasteners on the Front Spar
- Updated to add views for the removal and installation of hydraulic bracket
- Note added to avoid clash between the fasteners during removal or installation of fasteners
- Updated Fastener table to remove PNs EN6115V4-8, EN6115V6-14, ASNA2531-4 and ASNA2531-6.
A350-A-57-XX-P069- 03002-920A-A Replace the Fasteners on the Rear Spar, LH Side
- Warning and cautions are added
- Added sentence in Standard Practices for fastener hole diameters and drill data in composite and hybrid structure
- Updated the word area with outer CWB
- Note updated for the torque value
- CML added
- MP reference added for electrical bonding step
- Wording updated for the procedure step.
Fig.BE Sol.AB Replacement of the Fasteners on the Rear Spar, LH Side Illustration is updated to replace the bonding code "P1" with "_1B3M2".
Fig.BI Sol.AA Removal/ Installation of the Fittings on the Rear Spar, LH Side
- Note updated for the torque value A350-A-57-XX-P069- 02002-920A-A Replace the Fasteners on the Front Spar, RH Side
- Added sentence in Standard Practices for fastener hole diameters and drill data in composite and hybrid structure
- Caution added
- Updated the word area with outer CWB
- CML added
- MP reference added for electrical bonding step
- Steps added for the removal and installation of hydraulic bracket to gain access to bracket item (20).
Fig.BB Sol.AB Replacement of the fasteners on the Front Spar
- Updated to add views for the removal and installation of hydraulic bracket
- Note added to avoid clash between the fasteners during removal or installation of fasteners
- Updated Fastener table to remove PNs EN6115V4-8, EN6115V6-14, ASNA2531-4 and ASNA2531-6.
A350-A-57-XX-P069- 04002-920A-A Replace the Fasteners on the Rear Spar, RH Side
- Warning and cautions are added
- Added sentence in Standard Practices for fastener hole diameters and drill data in composite and hybrid structure
- Updated the word area with outer CWB
- Note updated for the torque value
- CML added
- MP reference added for electrical bonding step
A350
SERVICE BULLETIN
REVISION TRANSMITTAL SHEET REV 00 Nov 16/21 A350-57-P069 REV 01 Jun 07/24 Page 11
- Wording updated for the procedure step.
Fig.BD Sol.AB Replacement of the Fasteners on the Rear Spar, RH Side Illustration is updated to replace the bonding code "P1" with "_1B3M2".
Fig.BH Sol.AA Removal/ Installation of the Fittings on the Rear Spar, RH Side
- Note updated for the torque value.
T ask A350-A-57-XX-P069-02001-900A-C On Bench, Ream the Fittings Fig.BJ Sol.AB Ream the Fittings Illustration is updated to add note
CONF ALL D. FILING INSTRUCTIONS This Service Bulletin has been generated electronically and is reissued as a complete document. Replace the complete document.
Put this Revision Transmittal Sheet in front of the Service Bulletin.
E. HISTORY OF PREVIOUS REVISIONS No previous revision F. REVISION SEQUENCE ORIGINAL: Nov 16/21 REVISION No. : 01 - Jun 07/24
A350
SERVICE BULLETIN
SUMMARY REV 00 Nov 16/21 A350-57-P069 REV 01 Jun 07/24 Page 12 ATA SYSTEM: 57 TITLE: WINGS - CENTER WING - FASTENERS REPLACEMENT IN THE CENTER
WING BOX AT THE REAR SPAR AND THE FRONT SPAR LOWER AREA
SUMMARY This summary is for information only and is not approved for modification of the aircraft.
A. MODIFICATIONS CONF 001
MODIFICATION CLASSIFICATION MAJOR 116374L27002 116559L27019 MINOR 116810L27029 NOTE: As per EASA IR 21, a minor change is one that has no appreciable effect on the mass, balance, structural strength, reliability, operational characteristics affecting the airworthiness of the product. All other changes are major changes.
NOTE: This modification is related to an airworthiness issue and has been re-classified and confirmed by EASA as minor in accordance with EU Part 21.A.91. As such, this is handled by Airbus under the Design Organisation Approval ref. EASA.21J.031.
CONF 002
MODIFICATION CLASSIFICATION MAJOR 116374L27002 116559L27019 MINOR None NOTE: As per EASA IR 21, a minor change is one that has no appreciable effect on the mass, balance, structural strength, reliability, operational characteristics affecting the airworthiness of the product. All other changes are major changes.
CONF 003
MODIFICATION CLASSIFICATION MAJOR 116374L27002 116559L27019 MINOR 116810L27029 NOTE: As per EASA IR 21, a minor change is one that has no appreciable effect on the mass, balance, structural strength, reliability, operational characteristics affecting the airworthiness of the product. All other changes are major changes.
NOTE: This modification is related to an airworthiness issue and has been re-classified and confirmed by EASA as minor in accordance with EU Part 21.A.91. As such, this is handled by Airbus under the Design Organisation Approval ref. EASA.21J.031.