FAA 2015-25-04

Effective 2021-06-18 · Applies to: Leonardo 109

Cross-jurisdiction flags

Timing differs from EASA by 344 days
FAA effective 2021-06-18; EASA 2020-0142 effective 2020-07-09

Subject

The FAA is superseding Airworthiness Directive (AD) 2015-25-04 for Agusta S.p.A (now Leonardo S.p.a.) Model A109A and A109A II helicopters. AD 2015-25-04 required inspecting the slider assembly pitch control (slider) for play and replacing the slider if the play exceeds certain limits. This AD was prompted by further investigation that led to the determination that the play was caused by a manufacturing issue. This AD retains certain requirements of AD 2015- 25-04, requires replacing certain part-numbered sliders as a terminating action for the inspections, and prohibits installing the affected part on any helicopter. The FAA is issuing this AD to address the unsafe condition on these products.

Compliance time

Within 25 hours time-in-service (TIS) after the effective date of this AD, and thereafter at intervals not to exceed 25 hours TIS, inspect the slider for play.
Source: FAA · scraped 2026-06-21 04:02 UTC