SAE ARP4402 Eddy Current Inspection of Open Fastener Holes in Aluminum Aircraft Structure
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Product Code:SAE ARP4402
Title:Eddy Current Inspection of Open Fastener Holes in Aluminum Aircraft Structure
Issuing Committee:Ams K Non Destructive Methods And Processes Committee
Scope: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.
Title:Eddy Current Inspection of Open Fastener Holes in Aluminum Aircraft Structure
Issuing Committee:Ams K Non Destructive Methods And Processes Committee
Scope: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.
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