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2019-0138R1 : [Correction] Stabilizers – Elevators – Inspection

Number 2019-0138R1
Issued by Europe  Europe
Issue date 2022-05-09
Effective date 2022-05-16
EASA approval number
ATA Chapter 55
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 2019-0138 dated 12 June 2019.
Correction This AD is re-published to correct the Issue Date.
Supersedure The original issue of this AD superseded EASA AD 2009-0255 dated 01 December 2009.
Publication(s) and related information Airbus SB A330-55-3039 original issue dated 07 August 2009, Revision 01 dated 15 February 2019 and Revision 02 dated 13 April 2021. Airbus SB A340-55-4035 original issue dated 07 August 2009 and Revision 01 dated 15 February 2019. The use of later approved revisions of the above-mentioned documents is acceptable for compliance with the requirements of this AD.
PAD number 19-034
Remarks 1. If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD. 2. The original issue of this AD was posted on 07 March 2019 as PAD 19-034 for consultation until 04 April 2019. Revision 1 of this AD was posted on 04 March 2021 as PAD 21-063 for consultation until 18 May 2021. 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.