AD 2015-25-04
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Agusta | S.p.A. | Airworthiness Directives; Agusta S.p.A. Helicopters |
Unsafe Condition
Excessive play and wear on the slider assembly pitch control (slider) could lead to loss of tail rotor pitch control and consequently loss of helicopter control.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Inspect the slider assembly pitch control for play within 25 hours time-in-service (TIS) and thereafter at intervals not to exceed 25 hours TIS. Replace the slider with an airworthy one if play exceeds 2.3 millimeters (0.09 inch) before further flight.
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Compliance Time
Within 25 hours time-in-service (TIS)
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Affected Aircraft
Agusta S.p.A. Model A109A and A109A II helicopters.
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Source: Official FAA Source ↗
Retrieved: Apr 6, 2026
Rights: U.S. Government Public Domain
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