This SAE Aerospace Recommended Practice establishes the requirements and procedures for eddy current inspection of open fastener holes in aluminum aircraft structures.
Rationale
ARP4402A results from a Five-Year Review and update of this specification.
The committee of Nondestructive Methods and Processes, AMS Committee K, shall prepare, coordinate, and revise documents related to nondestructive testing technology, such as fluroescent penetrant, magnetic particle, X-ray, ultrasonic, and eddy current, through the participation of manufacturer's suppliers, users, and interested government agencies. Committee activities shall provide a forum for the cooperative interchange of ideas and experience of the participants, resulting in the publication of specifications that embody sound, established aerospace industry practices, and requirements to serve the suppliers and customers of aerospace materials.
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ARP4402A
Eddy Current Inspection of Open Fastener Holes in Aluminum Aircraft Structure
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Eddy Current Inspection of Open Fastener Holes in Aluminum Aircraft Structure
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