AD 2024-19-05
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Turbomeca | Makila 1A | Airworthiness Directives; Safran Helicopter Engines, S.A. (Type Certificate Previously Held by Turbomeca, S.A.) Engines |
| aircraft | Aviat | Various | Airworthiness Directives; Safran Helicopter Engines, S.A. (Type Certificate Previously Held by Turbomeca, S.A.) Engines |
| engine | Safran | Helicopter | Airworthiness Directives; Safran Helicopter Engines, S.A. (Type Certificate Previously Held by Turbomeca, S.A.) Engines |
Unsafe Condition
The accumulated service life of certain critical parts was underestimated, leading to potential operation beyond part life and failure of affected parts, possibly resulting in uncontained debris release.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Determine the recalculated service life of certain critical parts, replace the parts if necessary, and install the parts in accordance with specified conditions.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Within the compliance times specified in the referenced EASA AD.
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
Safran Helicopter Engines, S.A. (Type Certificate Previously Held by Turbomeca, S.A.) Model Makila 1A, Makila 1A1, and Makila 1A2 engines.
AI-generated summary from the source AD text. Verify against the official source before acting.
Source: Official FAA Source ↗
Retrieved: Apr 4, 2026
Rights: U.S. Government Public Domain
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