ARP4402A - Eddy Current Inspection of Open Fastener Holes in Aluminum Aircraft Structure

Details Not available for purchase at this time. Document Number: ARP4402A Project Initiation: 01-24-2013 Project Number: Revision Number: A Sponsor Name: Dorsey R. Perkins Title Eddy Current Inspection of Open Fastener Holes in Aluminum Aircraft Structure 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. Rationale ARP4402A is a Five Year Review and update of this specification.

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