EASA AD 2026-0166
Fuselage – Splice of Frame X5295 – Inspection
EASA Airworthiness Directive 2026-0166 is an airworthiness directive affecting Airbus Helicopters EC 225 LP models with specific Airbus Helicopters modifications. It addresses an issue with the upper splice plates at frame X5295, where the material was incorrectly recorded as steel instead of aluminium, potentially compromising structural integrity. The directive mandates inspection and corrective actions to ensure proper maintenance and safety compliance.