EASA AD 2024-0106
SUPERSEDED BY EASA AD 2024-0199
Summary
EASA Airworthiness Directive 2024-0106 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Airbus A319, A320, A321, A330, A350, and A380 aeroplanes. It addresses corrosion and cracking issues found on broadband antenna adapter plates and related components installed on these aircraft models. The directive mandates inspections and corrective actions to ensure continued airworthiness and safety.
What Changed
EASA Airworthiness Directive 2024-0106 introduces mandatory repetitive general visual inspections of the affected antenna adapter plates and associated parts, with corrective actions required if corrosion or cracks are detected. It also sets conditions for installation of these parts and requires reporting inspection results to Airbus. This AD is an interim measure pending further regulatory action.
Why It Matters
This directive is critical for aviation professionals as it addresses a potential safety risk that could lead to in-flight detachment of radome or antenna components, potentially damaging the tail section and affecting aircraft control. Operators, maintenance organizations, and compliance teams must implement these inspections to prevent safety incidents and ensure regulatory compliance.
What To Do
Operators of affected Airbus A319, A320, A321, A330, A350, and A380 aircraft must perform initial and repetitive general visual inspections of the broadband antenna adapter plates within the compliance times specified in the applicable Airbus and Panasonic service bulletins, with intervals not exceeding 36 months. Any detected corrosion or cracks must be corrected before the next flight. Inspection results must be reported to Airbus within 30 days. Installation of affected parts is allowed only if they are new, inspected within 36 months, or inspected before next flight after installation.