SAE ARP4402-1992
Eddy Current Inspection of Open Fastener Holes in Aluminum Aircraft Structure

Standard No.

SAE ARP4402-1992

Release Date

1992

Published By

Society of Automotive Engineers (SAE)

Status

Be replaced

Replace By

SAE ARP4402-2013

Latest

SAE ARP4402A-2020

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.

SAE ARP4402-1992 history

• 2020 SAE ARP4402A-2020 Eddy Current Inspection of Open Fastener Holes in Aluminum Aircraft Structure
• 2013 SAE ARP4402-2013 Eddy Current Inspection of Open Fastener Holes in Aluminum Aircraft Structure
• 1992 SAE ARP4402-1992 Eddy Current Inspection of Open Fastener Holes in Aluminum Aircraft Structure