Fuselage — Cabin / Cargo Compartment Parts — Inspection / Replacement [Wrong Material]
- Published
- Effective
- Deadline
- Replaces
- 2015-0236
AI-generated summary of the official EASA document. Verify against the PDF before acting.
What to do
Operators must perform a special detailed inspection of affected cabin and cargo compartment parts before the aircraft reaches six years from its date of manufacture. If any parts made from improper material are found, they must be replaced with serviceable parts before the six-year threshold. Additionally, for aircraft previously inspected under earlier service bulletin revisions, additional work must be completed before reaching twelve years from manufacture. Compliance with the latest Airbus service bulletins is required.
Summary
EASA Airworthiness Directive 2021-0100 is an airworthiness directive addressing inspection and replacement of certain cabin and cargo compartment parts on Airbus A380 aeroplanes. It applies specifically to Airbus A380-841, A380-842, and A380-861 models with specified manufacturer serial numbers. The directive mandates inspection of affected parts for improper aluminium alloy material and replacement if necessary to maintain structural integrity.
What changed
This directive supersedes EASA AD 2015-0236 and retains its requirements while introducing additional inspection work as specified in Airbus Service Bulletin A380-53-8100 Revision 03. It expands the inspection scope and requires additional work for certain cabin parts to ensure correct identification of material. The directive updates compliance instructions to reflect the latest service bulletin revisions.
Why it matters
This directive is critical for maintaining the structural integrity of affected Airbus A380 aircraft by ensuring that parts made from improper aluminium alloy are identified and replaced. Operators, maintenance organizations, and compliance teams must adhere to these requirements to prevent potential safety risks. Failure to comply could result in operating aircraft with compromised structural components, affecting airworthiness and safety.
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