Superseded by EASA AD 2025-0107
Superseded. Comply with 2025-0107, which replaces this document.
- Published
- Effective
AI-generated summary of the official EASA document. Verify against the PDF before acting.
What to do
Affected stakeholders should discontinue reliance on this superseded directive and consult EASA AD 2025-0107 for the latest instructions. They should ensure all maintenance, inspections, and operational procedures align with the new directive to maintain airworthiness and regulatory compliance.
Summary
EASA Airworthiness Directive SUPERSEDED BY EASA AD 2025-0107 concerns the Airbus S.A.S. A321 aircraft. This directive has been officially replaced by EASA AD 2025-0107 and no longer applies. Due to the document content being unavailable, specific technical details cannot be provided.
What changed
This document has been superseded by EASA AD 2025-0107, indicating that the previous requirements or instructions have been updated or replaced by the new directive. Operators should refer to EASA AD 2025-0107 for the current regulatory requirements.
Why it matters
For aviation professionals, this means that compliance and maintenance activities should now follow the updated guidance in EASA AD 2025-0107. Using outdated directives could lead to non-compliance and potential safety risks.
More for Airbus A321
All 285- EASA PAD 26-123Fuselage – Forward Fuselage Skin Panels – InspectionOct 13, 2026
- EASA PAD 26-113Engine – High Pressure Turbine Front Seal – InspectionSep 23, 2026
- EASA AD 2026-0182R1Stabilizers – Elevators – Inspections / ReplacementSep 22, 2026
- EASA AD 2026-0182Stabilizers – Elevators – Inspections / ReplacementSep 21, 2026
- EASA AD 2026-0176Electrical Systems Installation – Battery Retaining Rods – Identification / ReplacementSep 11, 2026
Get the next one by email
New ADs and bulletins for Airbus A321, summarized like this page, every Monday.