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SAE ARP 4402:2013-06-11

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SAE ARP 4402:2013-06-11

Eddy Current Inspection of Open Fastener Holes in Aluminum Aircraft Structure

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This SAE Aerospace Recommended Practice establishes the requirements and procedures for eddy current inspection of open fastener holes in aluminum aircraft structures.
Author SAE
Editor SAE
Document type Standard
Format File
Confirmation date 2013-06-11
ICS 49.030.01 : Fasteners in general
Number of pages 16
Set AEROPAKS10U-10
Year 2013
Document history
Country USA
Keyword SAE 4402;SAE ARP4402;SAE ARP4402;SAE ARP 4402