EASA AD 2020-0005R1
Fuselage — Windshield Central Lower Node Continuity Fittings — Inspection / Modification
EASA Airworthiness Directive 2020-0005R1 is an updated regulatory document addressing inspection and modification requirements for the windshield central lower node continuity fittings on Airbus A318, A319, A320, and A321 aircraft. It mandates repetitive high frequency eddy current inspections and corrective actions to detect and repair fatigue cracks in these fittings to prevent potential structural failure and decompression risks. The directive applies to specific aircraft configurations excluding those with certain Airbus modifications embodied in production or service.