Safety Publications Tool

2022-0067 : Time Limits / Maintenance Checks – Airworthiness Limitations Section – Amendment

Number 2022-0067
Issued by Europe  Europe
Issue date 2022-04-13
Effective date 2022-04-27
EASA approval number
ATA Chapter 04
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 Not applicable
Correction Not applicable
Supersedure This AD supersedes EASA AD 2017-0243 dated 06 December 2017, EASA AD 2018-0168R1 dated 18 December 2020 and EASA AD 2018-0284 dated 20 December 2018.
Publication(s) and related information AH "EC135 P1, P2, P3, T1, T2, T3, limited to CDS, CPDS, P2+, T2+, Chapter 04, Airworthiness Limitations Section", Revision 002 dated 06 April 2021. AH "EC135 P3H, T3H Chapter 04, Airworthiness Limitations Section", Revision 002 dated 06 April 2021. The use of later approved revisions of the above-mentioned documents is acceptable for compliance with the requirements of this AD.
PAD number 22-025
Remarks 1. If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD. 2. This AD was posted 14 March 2022 as PAD 22-025 for consultation until 11 April 2022. No comments were received during the consultation period. 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.