2023-16-04
FR doc 2023-17575 · 88 FR 55362AD 2023-16-04Published 2023-08-15Effective 2023-08-30
Requires repetitively inspecting the HTTA fitting assembly for corrosion and cracking until the HTTA fitting assembly is replaced with a new part.
Full official abstract
The FAA is adopting a new airworthiness directive (AD) for certain Piaggio Aviation S.p.A. (Piaggio) Model P-180 airplanes. This AD was prompted by a report of corrosion-induced cracking on the horizontal tail trim actuator (HTTA) fitting assembly. This AD requires repetitively inspecting the HTTA fitting assembly for corrosion and cracking until the HTTA fitting assembly is replaced with a new part. The FAA is issuing this AD to address the unsafe condition on these products.
More directives for Piaggio P.180 Avanti
- AD 2026-06-05 Airworthiness Directives; Baykar Piaggio Aerospace S.p.A. (Type Certific... Effective 2026-05-11
- AD 2026-05-10 Airworthiness Directives; Baykar Piaggio Aerospace S.p.A. (Type Certific... Effective 2026-04-27
- AD 2025-26-05 Airworthiness Directives; Baykar Piaggio Aerospace S.p.A. (Type Certific... Effective 2026-02-17
- AD 2025-15-10 Airworthiness Directives; Piaggio Aviation S.p.A. Airplanes Effective 2025-09-03
- AD 2023-25-03 Airworthiness Directives; Piaggio Aviation S.p.A. Airplanes Effective 2024-02-02
