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Rule. "Airworthiness Directives; Safran Helicopter Engines, S.A. (Type Certificate Previously Held by Turbomeca, S.A.) Engines" Federal Register 89, no. 204 (October 22, 2024): 84272-84274. https://www.govinfo.gov/app/details/FR-2024-10-22/2024-24365.
Office of the Federal Register, National Archives and Records Administration. (). 89 FR 84272 - Airworthiness Directives; Safran Helicopter Engines, S.A. (Type Certificate Previously Held by Turbomeca, S.A.) Engines. [Government]. Office of the Federal Register, National Archives and Records Administration. https://www.govinfo.gov/app/details/FR-2024-10-22/2024-24365
Office of the Federal Register, National Archives and Records Administration. 89 FR 84272 - Airworthiness Directives; Safran Helicopter Engines, S.A. (Type Certificate Previously Held by Turbomeca, S.A.) Engines. Office of the Federal Register, National Archives and Records Administration, , https://www.govinfo.gov/app/details/FR-2024-10-22/2024-24365
Office of the Federal Register, National Archives and Records Administration, Airworthiness Directives; Safran Helicopter Engines, S.A. (Type Certificate Previously Held by Turbomeca, S.A.) Engines, govinfo, (October 22, 2024), https://www.govinfo.gov/app/details/FR-2024-10-22/2024-24365.
Close xFederal Register Volume 89, Issue 204 (October 22, 2024)
Regulatory Information
Federal Register
AE 2.7:
GS 4.107:
AE 2.106:
Office of the Federal Register, National Archives and Records Administration
Rules and Regulations
Final rule.
This AD is effective November 26, 2024.
David Bergeron, Aviation Safety Engineer, FAA, 1600 Stewart Avenue, Suite 410, Westbury, NY 11590; phone: (860) 386-1805; email: David.J.Bergeron@faa.gov.
The FAA is adopting a new airworthiness directive (AD) for all Safran Helicopter Engines, S.A. (Safran) (type certificate previously held by Turbomeca, S.A.) Model Makila 1A, Makila 1A1, and Makila 1A2 engines. This AD is prompted by a determination that the accumulated service life of certain critical parts was underestimated. This AD requires determining the recalculated service life of certain critical parts, replacing if necessary, and also specifies conditions for installing the parts, as specified in a European Union Aviation Safety Agency (EASA) AD, which is incorporated by reference. The FAA is issuing this AD to address the unsafe condition on these products.
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
84272-84274
89 FR 84272
2120-AA64
14 CFR 39
Air Transportation; Aircraft; Aviation Safety; Incorporation by Reference and Safety
Docket No. FAA-2024-1691, Project Identifier MCAI-2023-01269-E, Amendment 39-22847, AD 2024-19-05
2024-24365