Fuselage – Belly Fairing Torsion Box – Modification
Superseded. Comply with 2022-0100, which replaces this document.
- Published
- Effective
AI-generated summary of the official EASA document. Verify against the PDF before acting.
What to do
Operators of affected Airbus A380 aircraft must modify the belly fairing torsion box parts in accordance with Airbus Service Bulletin A380-53-8153 within 147 months from the aircraft's date of manufacture. Maintenance teams should follow the detailed instructions in the service bulletin and document compliance accordingly. Requests for alternative methods of compliance can be submitted to EASA if substantiated.
Summary
EASA Airworthiness Directive 2019-0222 is an airworthiness directive issued for Airbus A380 aeroplanes, specifically models A380-841, A380-842, and A380-861 with certain manufacturer serial numbers. The directive addresses cracks found in the belly fairing torsion box parts on both left-hand and right-hand sides of the fuselage. It mandates modification of these parts to ensure continued airworthiness and safety.
What changed
EASA Airworthiness Directive 2019-0222 introduces a mandatory modification of the belly fairing torsion box on affected Airbus A380 aircraft to an improved design as specified in Airbus Service Bulletin A380-53-8153. This modification is required to prevent potential in-flight loss of the affected parts and to allow the aircraft to reach its design service goal.
Why it matters
This directive is critical for aviation professionals because it addresses a structural safety issue that could lead to loss of control of the aircraft if not corrected. Operators and maintenance organizations must ensure compliance to maintain aircraft airworthiness and avoid operational disruptions. Compliance also ensures adherence to European Union aviation safety regulations.
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