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  Safety Publications Tool

2022-0190 : Nacelles / Pylons – Lower Aft Pylon Fairings – Inspection

Number 2022-0190
Issued by Europe  Europe
Issue date 2022-09-14
Effective date 2022-09-28
EASA approval number
ATA Chapter 54
Approval Holder
/ Type Designation
  • AIRBUS S.A.S.
    • A330
      • A330-223
      • A330-321
      • A330-322
      • A330-323
Revision Not applicable
Correction Not applicable
Supersedure This AD supersedes DGAC France AD F-2004-028R2 (EASA approval 2005-6373) dated 26 October 2005.
Publication(s) and related information Airbus SB A330-54-3021 original issue dated 04 February 2004, Revision 01 dated 16 June 2004 and Revision 02 dated 28 January 2008. Airbus SB A330-54-3022 original issue dated 25 May 2005 and Revision 01 dated 09 January 2008. Airbus SB A330-54-3050 original issue dated 08 November 2021. The use of later approved revisions of the above-mentioned documents is acceptable for compliance with the requirements of this AD.
PAD number 22-105
Remarks 1. If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD. 2. This AD was posted on 01 August 2022 as PAD 22-105 for consultation until 29 August 2022. The 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 Safety 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. This may include reporting on the same or similar components, other than those covered by the design to which this AD applies, if the same unsafe condition can exist or may develop on an aircraft with those components installed. Such components may be installed under an FAA Parts Manufacturer Approval (PMA), Supplemental Type Certificate (STC) or other modification.