Wing — Main Landing Gear Retraction Actuator Fitting — Inspection
- Published
- Effective
- Replaces
- 2007-0162
- Replaces
- 2014-0169
- Replaces
- 2025-0254
AI-generated summary of the official EASA document. Verify against the PDF before acting.
What to do
Affected operators must perform detailed inspections of the wing inner rear spars and main landing gear actuator fittings within specified flight hour or cycle thresholds and at recurring intervals. For Group 3 aeroplanes, a modification per Airbus SB A320-57-1089 Revision 04 must be completed before exceeding 48,000 flight cycles or 96,000 flight hours. Any discrepancies found during inspections require contacting Airbus for approved repair instructions and prompt corrective action. Compliance deadlines vary by aircraft group and are detailed within the directive.
Summary
EASA Airworthiness Directive 2025-0254R1 is an updated safety directive addressing inspection requirements for the main landing gear retraction actuator fitting on the rear spar of Airbus A320 and A321 aeroplanes. It applies to specific A320 and A321 models except those modified with certain Airbus service bulletins or modifications. The directive mandates detailed inspections and corrective actions to detect and repair fatigue cracks and corrosion that could compromise structural integrity.
What changed
This revision updates paragraphs (1), (7), and (8) of the original AD 2025-0254 to clarify applicability and inspection requirements, including exemptions for certain Group 1 aeroplanes with specific service bulletins embodied. It also prohibits the use of Airbus SB A320-57-1089 at revisions lower than Revision 04 for Group 3 aeroplanes and incorporates feedback received during the consultation period.
Why it matters
This directive is critical for maintaining the structural integrity of affected Airbus A320 and A321 aircraft by addressing fatigue cracks and corrosion in the main landing gear actuator fittings. Operators, maintenance organizations, and compliance teams must adhere to these updated inspection intervals and modification requirements to prevent potential fuel leaks and structural failures, ensuring continued airworthiness and safety.
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