AD 2025-10-10
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Pilatus | Aircraft Ltd | Airworthiness Directives; Pilatus Aircraft Ltd. Airplanes |
Unsafe Condition
Variations in the microstructure of certain batches of titanium threaded bolts could affect their fatigue characteristics, leading to failure of the bolts with consequent damage to the rudder and rudder trim tab, which could result in loss of rudder control and reduced or loss of control of the airplane.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Replace affected short rudder-trim control rod assemblies with serviceable rudder-trim control rod assemblies having threaded steel bolts. Prohibit the installation of affected parts.
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Compliance Time
Before further flight
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Affected Aircraft
Pilatus Aircraft Ltd. Model PC-24 airplanes, certificated in any configuration.
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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