FAA 2024-15-11
Effective 2024-10-21
· Applies to:
Leonardo 109
Cross-jurisdiction flags
Timing differs from EASA by 503 days
FAA effective 2024-10-21; EASA 2023-0105 effective 2023-06-06
Cross-references
EASA
2023-0105
EASA AD 2023-0105
Subject
The FAA is adopting a new airworthiness directive (AD) for all Leonardo S.p.a. Model A109C, A109E, A109K2, A109S, and AW109SP helicopters. This AD was prompted by reports of loose tail rotor duplex bearing locking nuts, possibly caused by improper installation. This AD requires disassembling certain tail rotor duplex bearings and reassembling them in accordance with updated procedures. This AD also prohibits installing certain tail rotor duplex bearing housings and pitch change slider assemblies. 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.
Compliance time
within 100 hours time-in-service or 6 months, whichever occurs first.
Source: FAA · scraped 2026-06-21 04:02 UTC