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
22.09.2020
Aufsatz (Konferenz)
Englisch
Eddy Current Inspection of Open Fastener Holes in Aluminum Aircraft Structure
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