AD 2000-08-05
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Agusta | Model A109C and A109K2 | Airworthiness Directives; Agusta Model A109C and A109K2 Helicopters |
Unsafe Condition
Failure of a main rotor pitch control link rod-end spherical bearing, increased vibration level, and subsequent reduced controllability of the helicopter.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Rework each main rotor pitch control link assembly, P/N 109-0110-71-103 or -105, and reidentify as pitch control link assembly, P/N 109-0110-71-107, in accordance with Agusta Bollettino Tecnico 109K-10 or 109-103, dated November 22, 1995.
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Compliance Time
Before further flight, unless accomplished previously.
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Affected Aircraft
Agusta Model A109C and A109K2 helicopters with main rotor pitch control link assemblies, part number (P/N) 109-0110-71-103 or -105, installed.
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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