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2020-0283 : SUPERSEDED BY EASA AD 2022-0197

Number 2020-0283
Issued by Europe  Europe
Issue date 2020-12-24
Effective date 2020-12-31
EASA approval number
ATA Chapter 28
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
      • A330-743L (BelugaXL)
      • A330-841
      • A330-941
    • A340
      • A340-211
      • A340-212
      • A340-213
      • A340-311
      • A340-312
      • A340-313
      • A340-541
      • A340-542
      • A340-642
      • A340-643
Revision Not applicable
Correction This AD is republished to insert regulatory references, which were inadvertently omitted.
Supersedure This AD supersedes EASA AD 2019-0291R1 dated 04 March 2020.
Publication(s) and related information Airbus AOT A28L006-17 original issue dated 03 November 2017, or Revision 01 dated 16 November 2017, or Revision 02 dated 08 February 2018, or Revision 03 dated 28 May 2019, or Revision 04 dated 04 September 2019, or Revision 05 dated 02 March 2020, or Revision 06 dated 17 November 2020. Airbus SB A330-28-3132 original issue dated 06 March 2019, or Revision 01 dated 05 December 2019, or Revision 02 dated 09 July 2020. Airbus SB A340-28-4142 original issue dated 06 March 2019, or Revision 01 dated 28 April 2020. Airbus SB A340-28-5062 original issue dated 06 March 2019, or Revision 01 dated 28 April 2020. Eaton Aerospace Ltd SB 8810-28-06 Revision 2 dated 01 March 2019. The use of later approved revisions of the above-mentioned documents is acceptable for compliance with the requirements of this AD.
PAD number 20-186
Remarks 1. If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD. 2. This AD was posted on 24 November 2020 as PAD 20-186 for consultation until 08 December 2020. 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. 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.