AD Amdt-39-10907
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Agusta | A109C | Airworthiness Directives; Agusta A109C Helicopters |
Unsafe Condition
Cracks found on tail rotor blade grip assemblies could result in separation of a tail rotor blade and subsequent loss of control of the helicopter.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Replace the tail rotor blade grip assemblies with modified airworthy grip assemblies.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Within 5 hours time-in-service (TIS).
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
Agusta A109C helicopters.
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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