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SAE ARP4402

SAE ARP4402

SAE ARP4402 Eddy Current Inspection of Open Fastener Holes in Aluminum Aircraft Structure

standard by SAE International, 06/11/2013

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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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Published: 06/11/2013 File Size: 1 file , 580 KB

 
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