Superseded by EASA AD 2024-0009
Superseded. Comply with 2024-0009, which replaces this document.
- Published
- Effective
- Deadline
- Replaces
- 2020-0111R1
AI-generated summary of the official EASA document. Verify against the PDF before acting.
What to do
Operators must perform repetitive special detailed inspections of designated inspection areas within specified compliance times based on aircraft group and flight cycle or hour thresholds. If discrepancies are found, Airbus-approved corrective instructions must be followed before further flight. Compliance deadlines vary by aircraft group, with some inspections required before exceeding 17,200 flight cycles or within 27 days after 3 June 2020.
Summary
EASA Airworthiness Directive 2020-0111R2 is an updated safety directive affecting all certified Airbus A300-600 aeroplanes. It mandates repetitive special detailed inspections of specific structural areas including the outer wing bottom skin and fuselage internal structure to detect cracks that could compromise structural integrity. The directive ensures continued airworthiness by requiring compliance with Airbus Airworthiness Limitations Section tasks.
What changed
This revision corrects typographical errors in task numbers, updates inspection area references, replaces certain modification references with Airbus Service Bulletin A300-57-6123, and refines group definitions and related compliance instructions. It also introduces grace periods and clarifies compliance intervals for inspections across different aircraft groups.
Why it matters
This directive is critical for operators and maintenance organizations to prevent structural failures caused by undetected cracks in key airframe areas. Compliance ensures the safety and reliability of Airbus A300-600 aircraft by mandating timely inspections and corrective actions. It also helps avoid regulatory non-compliance and potential grounding of aircraft.
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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