EASA Regulations for Lavia PA-25 (Chincul)

2 airworthiness directives and regulations affecting Lavia PA-25 (Chincul).

EASA AD 2025-0154R1

Aircraft Flight Manual - Limitation / Wings — Front and Rear Spar — Inspections

The document titled Aircraft Flight Manual - Limitation / Wings — Front and Rear Spar — Inspections is an EASA Airworthiness Directive 2025-0154R1 issued on 7 August 2025. It applies to LAVIA ARGENTINA S.A. PA-25, PA-25-235, and PA-25-260 aeroplanes and mandates inspections of specific front and rear wing spars identified by part numbers. The directive addresses corrosion and crack findings in wing spars and related fittings to ensure continued airworthiness.

Aug 7, 2025

Airworthiness DirectiveMaintenanceSafety MgmtLavia PA-25 (Chincul)Lavia PA-25 (Pawnee)Lavia PA-25 (Puelche)

EASA AD RA-2024-05-01R1

NOT ADOPTED - EASA DECISION ATTACHED - SEE EASA AD 2025-0154

The document titled NOT ADOPTED - EASA DECISION ATTACHED - SEE EASA AD 2025-0154 is an official EASA position regarding the ANAC Argentina Airworthiness Directive RA 2024-05-01 and its Revision 1. It concerns LAVIA SA PA-25, PA-25-235, and PA-25-260 aeroplanes, addressing corrosion and crack findings in the front and rear spars and the drag wire pull fitting (P/N 61212-00) of the front spar. EASA decided not to adopt the ANAC Argentina AD and instead issued its own AD 2025-0154 to address the same unsafe condition with a different inspection regime and operational limitations.

Jan 27, 2025

Airworthiness DirectiveMaintenanceSafety MgmtLavia PA-25 (Chincul)Lavia PA-25 (Pawnee)Lavia PA-25 (Puelche)