SAE ARP 4402A:2020-09-22

SAE ARP 4402A:2020-09-22

Eddy Current Inspection of Open Fastener Holes in Aluminum Aircraft Structure

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Details

This SAE Aerospace Recommended Practice establishes the requirements and procedures for eddy current inspection of open fastener holes in aluminum aircraft structures.

Additional Info

Author Society of Automotive Engineers International (SAE)
Committee AMS K Non Destructive Methods and Processes Committee
Published by SAE
Document type Standard
ICS 49.030.01 : Fasteners in general
Number of pages 23
Replace SAE ARP 4402:2013-06-11
Document history SAE ARP 4402:2013-06-11
Keyword SAE 4402,SAE ARP4402A,SAE ARP4402A,SAE ARP 4402