Safety Publications Tool

2019-0122 : Fuselage – Side Box Beam Flange in Frame 43 Area – Inspection / Repair / Modification

Number 2019-0122
Issued by Europe  Europe
Issue date 2019-06-04
Effective date 2019-06-18
EASA approval number
ATA Chapter 53
Approval Holder
/ Type Designation
  • AIRBUS S.A.S.
    • A318
      • A318-111
      • A318-112
      • A318-121
      • A318-122
    • A319
      • A319-111
      • A319-112
      • A319-113
      • A319-114
      • A319-115
      • A319-131
      • A319-132
      • A319-133
    • A320
      • A320-211
      • A320-212
      • A320-214
      • A320-215
      • A320-216
      • A320-231
      • A320-232
      • A320-233
    • A321
      • A321-111
      • A321-112
      • A321-131
      • A321-211
      • A321-212
      • A321-213
      • A321-231
      • A321-232
Revision Not applicable
Correction Not applicable
Supersedure This AD supersedes EASA AD 2013-0261 dated 28 October 2013.
Publication(s) and related information Airbus SB A320-53-1258 original issue dated 18 October 2012, or Rev. 01 dated 27 June 2016, or Rev. 02 dated 07 September 2016. Airbus SB A320-53-1251 original issue dated 16 November 2012, or Rev. 01 dated 18 October 2013, or Rev. 02 dated 11 February 2016, or Rev. 03 dated 19 September 2016, or Rev. 04 dated 17 May 2019. Airbus A318/A319/A320/A321 ALS Part 2 Rev. 07 dated 13 June 2018. The use of later approved revisions of the above-mentioned documents is acceptable for compliance with the requirements of this AD.
PAD number 18-014
Remarks 1. If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD. 2. This AD was posted on 02 February 2018 as PAD 18-014 for consultation until 02 March 2018. The Comment Response Document can be found in the EASA Safety Publications Tool, in the compressed (zipped) file attached to the record for this AD. 3. Enquiries regarding this AD should be referred to the EASA Programming and Continued Airworthiness Information Section, Certification Directorate. E-mail: ADs[at]easa.europa.eu. 4. Information about any failures, malfunctions, defects or other occurrences, which may be similar to the unsafe condition addressed by this AD, and which may occur, or have occurred on a product, part or appliance not affected by this AD, can be reported to the EU aviation safety reporting system.