Safety Publications Tool
2022-0223 : Time Limits / Maintenance Checks – Airworthiness Limitations Section – Amendment
EASA approval number
EASA Environment & Propulsion Systems Department
/ Type Designation
SAFRAN HELICOPTER ENGINES
This AD supersedes EASA AD 2009-0017 dated 23 January 2009.
Publication(s) and related information
SAFRAN Makila 2A reference X 298 N7 460 2 MM ALS Update 16 dated 30 August 2022. The use of later approved revisions of the above-mentioned document is acceptable for compliance with the requirements of this AD.
1. If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD. 2. This AD was posted on 20 October 2022 as PAD 22-137 for consultation until 17 November 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.
EASA_AD_2022_0223.pdf (200 kb)
EASA_PAD_22_137.zip (378 kb)
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