Historical
SAE ARP 4402-1992 (SAE ARP4402-1992)
Eddy Current Inspection of Open Fastener Holes in Aluminum Aircraft Structure ( Reaffirmed: Jan 1996 Jul 1996 Feb 2007 )
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.
CONTENT PROVIDER
Society of Automotive Engineers [sae]
Society of Automotive Engineers [sae]