EASA AD 2018-0276R1
[Correction] Fuselage — Structural Parts / Joints — Modification / Reinforcement
Summary
EASA Airworthiness Directive 2018-0276R1 is a corrective revision addressing structural modifications and reinforcements for Airbus A330 series aeroplanes. It applies to multiple A330 variants including A330-200, A330-200F, and A330-300 models, focusing on fuselage structural parts and joints to prevent widespread fatigue damage. The directive mandates compliance with specific Airbus Service Bulletins to ensure continued airworthiness.
What Changed
This revision clarifies compliance times for certain modifications, particularly for Action 9 where previous revisions of Airbus SB A330-53-3238 were used. It also corrects an error in the compliance time for Action 14 and updates notes to better define applicability by aircraft configuration rather than just manufacturer serial numbers. The directive retains prior requirements while introducing new modifications for A330-200F aeroplanes and amending compliance schedules.
Why It Matters
This directive is critical for maintaining the structural integrity of Airbus A330 aircraft by addressing potential widespread fatigue damage that could lead to rapid depressurisation. Operators, maintenance organizations, and compliance teams must ensure timely modifications to prevent safety risks and regulatory non-compliance. Adhering to these requirements helps avoid structural failures and ensures continued safe operation of affected aircraft.
What To Do
Affected operators must perform the required structural modifications before exceeding specified Structural Modification Points, following the instructions in the referenced Airbus Service Bulletins. Alternative methods of compliance are allowed if approved by EASA. Compliance deadlines vary by aircraft configuration and modification action, with the effective date of this directive being 2019-01-13.
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