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2018-0168R1 : SUPERSEDED BY EASA AD 2022-0067

Number 2018-0168R1
Issued by Europe  Europe
Issue date 2020-12-18
Effective date 2020-12-25
EASA approval number
ATA Chapter 64
Approval Holder
/ Type Designation
  • AIRBUS HELICOPTERS DEUTSCHLAND
    • EC135/635
      • EC135 P1
      • EC135 P2
      • EC135 P2+
      • EC135 P3
      • EC135 T1
      • EC135 T2
      • EC135 T2+
      • EC135 T3
      • EC635 P2+
      • EC635 P3
      • EC635 T1
      • EC635 T2+
      • EC635 T3
Revision This AD revises EASA AD 2018-0168 dated 27 July 2018.
Correction Not applicable
Supersedure None
Publication(s) and related information AH ASB EC135-04A-013 original issue dated 26 June 2018. AH ASB EC135H-04A-001 original issue dated 26 June 2018. AH ASB EC135-64A-006 original issue dated 20 February 2018 and Revision 1 dated 21 October 2020. AH ASB EC135H-64A-001 original issue dated 20 February 2018 and Revision 1 dated 21 October 2020. The use of later approved revisions of the above-mentioned documents is acceptable for compliance with the requirements of this AD.
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 09 April 2018 as PAD 18-049 for consultation until 07 May 2018, and republished on 27 June 2018 as PAD 18-049R1 for additional consultation until 25 July 2018. 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 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.