AD 2024-10-14
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Aviat | Various | Airworthiness Directives; Rolls-Royce Deutschland Ltd & Co KG |
Unsafe Condition
Cracking and separation of certain low-pressure turbine (LPT) stage 1 blade assemblies.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Inspect affected LPT stage 1 blade assemblies for cracking or separation. Depending on inspection results, reduce inspection interval or replace the LPT stage 1 blade set and disk. Prohibit installation of an LPT disk or blade set assembly unless it is considered a serviceable part as specified in an EASA AD.
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Compliance Time
Within 50 flight hours after the effective date.
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Affected Aircraft
Rolls-Royce Deutschland Ltd & Co KG Trent 1000-A, Trent 1000-AE, Trent 1000-C, Trent 1000-CE, Trent 1000-D, Trent 1000-E, Trent 1000-G, and Trent 1000-H engines.
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Source: Official FAA Source ↗
Retrieved: Apr 6, 2026
Rights: U.S. Government Public Domain
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