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SAE ARP4402

(R) Eddy Current Inspection of Open Fastener Holes in Aluminum Aircraft Structure

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Organization: SAE
Publication Date: 1 September 2020
Status: active
Page Count: 23
scope:

Purpose

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

Application

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.

Document History

SAE ARP4402
September 1, 2020
(R) Eddy Current Inspection of Open Fastener Holes in Aluminum Aircraft Structure
Purpose This SAE Aerospace Recommended Practice establishes the requirements and procedures for eddy current inspection of open fastener holes in aluminum aircraft structures. Application This...
April 1, 1992
Eddy Current Inspection of Open Fastener Holes in Aluminum Aircraft Structure
Purpose: This SAE Aerospace Recommended Practice establishes the requirements and procedures for eddy current inspection of open fastener holes in aluminum aircraft structures. Applications: This...
April 1, 1992
Eddy Current Inspection of Open Fastener Holes in Aluminum Aircraft Structure
Purpose: This SAE Aerospace Recommended Practice establishes the requirements and procedures for eddy current inspection of open fastener holes in aluminum aircraft structures. Application: This...
April 1, 1992
Eddy Current Inspection of Open Fastener Holes in Aluminum Aircraft Structure
Purpose: This SAE Aerospace Recommended Practice establishes the requirements and procedures for eddy current inspection of open fastener holes in aluminum aircraft structures. Applications: This...

References

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