Time Limits / Maintenance Checks – Airworthiness Limitations Section Part 2 / Damage Tolerant Airworthiness Limitation Items – Amendment
Superseded. Comply with 2024-0009, which replaces this document.
- Published
- Effective
- Deadline
AI-generated summary of the official EASA document. Verify against the PDF before acting.
What to do
Operators of Airbus A300-600 aeroplanes must comply with the reduced LOV specified in Airbus A300-600 ALS Part 2 Variation 3.6 starting from 1 December 2021. Within 12 months of this effective date, they must revise their approved Aircraft Maintenance Programme to incorporate the updated LOV. Compliance with these requirements is mandatory to continue operating the affected aircraft.
Summary
EASA Airworthiness Directive 2021-0258 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting all certified models of Airbus A300-600 aeroplanes. It mandates compliance with updated airworthiness limitations related to structural maintenance to ensure continued airworthiness and safety. This directive updates the Limit Of Validity (LOV) for structural components as specified in Airbus A300-600 Airworthiness Limitations Section Part 2 Variation 3.6.
What changed
EASA Airworthiness Directive 2021-0258 introduces a reduced Limit Of Validity (LOV) for Airbus A300-600 aeroplanes based on new engineering data to prevent widespread fatigue damage. It requires operators to comply with the LOV specified in the latest Variation 3.6 of the Airbus A300-600 ALS Part 2. This AD does not supersede previous ADs but adds new mandatory maintenance requirements.
Why it matters
This directive is critical for aviation professionals as it ensures the structural integrity and safety of Airbus A300-600 aircraft by updating maintenance limits to reflect the latest fatigue damage assessments. Operators and maintenance organizations must revise their maintenance programs to comply with the reduced LOV, preventing unsafe conditions and regulatory non-compliance. Failure to comply could lead to unsafe operations and regulatory penalties.
More for Airbus A300-600
All 62- EASA PAD 26-109Wings – Main Landing Gear Attachment / Rib 5 Forward Lug – Inspection(s)Sep 18, 2026
- EASA PAD 26-013Fuselage — Door Frames Holes — InspectionJan 26, 2026
- EASA AD 2018-0229R1Wings — Centre Wing Box Frame 47 Angle Fittings — Inspection / ModificationNov 20, 2025
- EASA AD 2025-0255Time Limits / Maintenance Checks — Airworthiness Limitations Section Part 2 / Damage Tolerant Airworthiness Limitations Items — AmendmentNov 19, 2025
- EASA AD 2025-0236
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