AD 2000-26-02
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Eurocopter | Deutschland Model EC135 P1 and T1 | Airworthiness Directives; Eurocopter Deutschland Model EC135 P1 and T1 Helicopters |
Unsafe Condition
Cracked stator blade of the fenestron tail rotor due to additional reports of cracking leading to tail rotor failure.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Replace existing stator blade assembly with a new assembly incorporating a reinforced base and modified riveting. Limit applicability to certain serial numbered tail booms.
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
Eurocopter Deutschland Model EC135 P1 and T1 helicopters with certain serial numbered tail booms.
AI-generated summary from the source AD text. Verify against the official source before acting.
Source: Official FAA Source ↗
Retrieved: Apr 6, 2026
Rights: U.S. Government Public Domain
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