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2018-0249R1 : [Correction] Wings – Centre Wing Box Fastener Holes at Frame 40 Vertical Web – Inspection / Modification

Number 2018-0249R1
Issued by Europe  Europe
Issue date 2019-08-02
Effective date 2019-08-30
EASA approval number
ATA Chapter 57
Approval Holder
/ Type Designation
  • AIRBUS S.A.S.
    • A330
      • A330-201
      • A330-202
      • A330-203
      • A330-223
      • A330-223F
      • A330-243
      • A330-243F
      • A330-301
      • A330-302
      • A330-303
      • A330-321
      • A330-322
      • A330-323
      • A330-341
      • A330-342
      • A330-343
    • A340
      • A340-211
      • A340-212
      • A340-213
      • A340-311
      • A340-312
      • A340-313
Revision This AD revises EASA AD 2018-0249 dated 16 November 2018.
Correction This AD is re-published to correct certain references to Notes.
Supersedure The original issue of this AD superseded EASA AD 2017-0069 dated 25 April 2017.
Publication(s) and related information Airbus SB A330-57-3114 original issue dated 12 March 2013, or Revision 01 dated 13 January 2017. Airbus SB A330-57-3115 original issue dated 04 April 2013, or Revision 01 dated 23 November 2016, or Revision 02 dated 29 May 2018. Airbus SB A330-57-3116 original issue dated 12 March 2013, or Revision 01 dated 23 November 2016, or Revision 02 dated 05 February 2018. Airbus SB A330-57-3129 original issue dated 05 October 2016, or Revision 01 dated 21 September 2017. Airbus SB A330-57-3130 original issue dated 23 November 2016, or Revision 01 dated 18 February 2018. Airbus SB A330-57-3131 original issue dated 23 November 2016, or Revision 01 dated 13 February 2018. Airbus SB A330-57-3132 original issue dated 23 November 2016, or Revision 01 dated 05 February 2018. Airbus SB A340-57-4123 original issue dated 12 March 2013, or Revision 01 dated 13 January 2017. Airbus SB A340-57-4124 original issue dated 04 April 2013, or Revision 01 dated 22 August 2013, or Revision 02 dated 23 November 2016, or Revision 03 dated 28 May 2018. Airbus SB A340-57-4125 original issue dated 12 March 2013, or Revision 01 dated 23 November 2016, or Revision 02 dated 25 April 2018. Airbus SB A340-57-4136 original issue dated 05 October 2016, or Revision 01 dated 27 September 2017. Airbus SB A340-57-4137 original issue dated 23 November 2016, or Revision 01 dated 27 September 2017. Airbus SB A340-57-4138 original issue dated 23 November 2016, or Revision 01 dated 13 February 2018. Airbus SB A340-57-4139 original issue dated 23 November 2016. Airbus OIT 999.0086/11 dated 9 November 2011. The use of later approved revisions of the above-mentioned documents is acceptable for compliance with the requirements of this AD.
PAD number 19-074
Remarks 1. If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD. 2. This revised AD was posted for consultation on 25 April 2019 as PAD 19-074 for consultation until 09 May 2019. The original issue of this AD was posted on 13 September 2018 as PAD 18-127 and republished on 26 September 2018 as PAD 18-127R1 for consultation until 11 October 2018. All Comment Response Documents 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.