Eddy Current Inspection of Open Fastener Holes in Aluminum Aircraft Structure.

Product Code: ARP4402

Date Published: 1992-04-01
Date Reaffirmed: February 2007

Issuing Committee:

Ams K Non Destructive Methods And Processes Committee

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.

Product Status: In Stock

File Size: 1582K

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Current & Historical versions of this standard
Standard	Date published	?Status
ARP4402	1992-04-01	Reaffirmed

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Eddy Current Inspection of Open Fastener Holes in Aluminum Aircraft Structure.

Issuing Committee:

Scope

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