SAE Standards Works
AMS K Non Destructive Methods and Processes Committee
ARP4402A - Eddy Current Inspection of Open Fastener Holes in Aluminum Aircraft Structure
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Dorsey R. Perkins
Eddy Current Inspection of Open Fastener Holes in Aluminum Aircraft Structure
This SAE Aerospace Recommended Practice establishes the requirements and procedures for eddy current inspection of open fastener holes in aluminum aircraft structures. This process has been used typically by maintenance and overhaul facilities personnel to inspect aluminum aircraft structures for service-induced cracks, but usage is not limited to such applications.
ARP4402A is a Five Year Review and update of this specification.