FAA 2024-17-07
Effective 2024-11-12
· Applies to:
Leonardo 139
Cross-jurisdiction flags
Timing differs from EASA by 756 days
FAA effective 2024-11-12; EASA 2022-0205 effective 2022-10-18
Cross-references
EASA
2022-0205
Tail rotor – damper bracket inspection on AW139 (origin AD; FAA adopted as 2024-17-07).
Subject
The FAA is adopting a new airworthiness directive (AD) for all Leonardo S.p.a. Model AB139 and AW139 helicopters. This AD was prompted by multiple reports of cracks found on tail rotor (TR) damper bracket assemblies. This AD requires accomplishing repetitive detailed visual inspections (DVIs) of certain part-numbered TR damper bracket assemblies for corrosion and cracks and, depending on the results, taking corrective action. This AD also prohibits installing an affected TR damper bracket assembly unless it is new. These actions are specified in a European Union Aviation Safety Agency (EASA) AD, which is incorporated by reference. The FAA is issuing this AD to address the unsafe condition on these products.
Source: FAA · scraped 2026-05-06 23:01 UTC