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  Safety Publications Tool

2024-0218 : Engine – Gas Generator High-Pressure Turbine Blades – Replacement

Number 2024-0218
Issued by Europe  Europe
Issue date 2024-11-18
Effective date 2024-12-02
EASA approval number
Contributor EASA Environment & Propulsion Systems Department
ATA Chapter 72
Approval Holder
/ Type Designation
  • SAFRAN HELICOPTER ENGINES
    • ARRIUS 2
      • ARRIUS 2F
      • ARRIUS 2R
Revision Not applicable
Correction Not applicable
Supersedure None
Publication(s) and related information SAFRAN SB 319 72 4853 version B dated 10 October 2024. The use of later approved revisions of the above-mentioned document is acceptable for compliance with the requirements of this AD.
PAD number 24-120
Remarks 1. If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD. 2. This AD was posted on 16 October 2024 as PAD 24-120 for consultation until 13 November 2024. 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.