Wings — Centre Section Frame 40 Forward Fitting Radius at Tension Bolt Junction — Inspection / Repair
- Published
- Effective
AI-generated summary of the official EASA document. Verify against the PDF before acting.
What to do
Affected operators and maintenance providers must perform the inspections and repairs as outlined in the directive within the specified compliance times. They should review the detailed procedures and schedule maintenance accordingly to meet regulatory requirements. No explicit compliance deadline is stated in the document text.
Summary
The document titled 'Wings — Centre Section Frame 40 Forward Fitting Radius at Tension Bolt Junction — Inspection / Repair' is an Airworthiness Directive issued by AIRBUS S.A.S. specifically for the Airbus A300-600 aircraft. It addresses inspection and repair requirements for the forward fitting radius at the tension bolt junction on the centre section frame 40 of the wing. The directive aims to ensure structural integrity and safety of the affected aircraft component.
What changed
This new Airworthiness Directive introduces mandatory inspection and repair procedures for the centre section frame 40 forward fitting radius at the tension bolt junction on Airbus A300-600 wings. It specifies detailed inspection methods and repair instructions to detect and address potential structural issues before they compromise safety.
Why it matters
This directive is critical for aviation professionals as it helps prevent structural failures that could impact flight safety. Operators and maintenance organizations must comply to maintain airworthiness and avoid costly unscheduled repairs or grounding. Compliance ensures continued safe operation of the Airbus A300-600 fleet.
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