Fuselage — Upper Frame Feet Fittings — Modification
- Published
- Effective
AI-generated summary of the official EASA document. Verify against the PDF before acting.
What to do
Affected operators and maintenance teams should review the modification instructions and implement the required changes to the upper frame feet fittings as specified. They must schedule and complete the modification within any stated compliance timeframe to remain compliant. Monitoring for any further updates or related directives is also advised.
Summary
Fuselage — Upper Frame Feet Fittings — Modification is a regulatory document concerning the Airbus A300-600 aircraft model. It addresses modifications related to the upper frame feet fittings of the fuselage structure. The document aims to ensure continued airworthiness and structural integrity of the affected aircraft.
What changed
This document introduces a modification requirement for the upper frame feet fittings on the fuselage of Airbus A300-600 aircraft. It specifies the necessary changes or upgrades to these fittings to maintain structural safety. The modification is intended to prevent potential issues related to frame fitting integrity.
Why it matters
This modification is critical for aviation professionals as it directly impacts the structural safety and airworthiness of the Airbus A300-600 fleet. Operators and maintenance organizations must be aware of these changes to ensure compliance and avoid potential safety risks. Compliance helps maintain aircraft reliability and regulatory adherence.
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- 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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