This SAE Aerospace Recommended Practice establishes the requirements and procedures for eddy current inspection of open fastener holes in aluminum aircraft structures. ARP4402A results from a Five-Year Review and update of this specification.
Eddy Current Inspection of Open Fastener Holes in Aluminum Aircraft Structure
2020-09-22
Conference paper
English
Eddy Current Inspection of Open Fastener Holes in Aluminum Aircraft Structure
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