SAE ARP4402 Rev A

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

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SAE ARP4402 Rev A

Eddy Current Inspection of Open Fastener Holes in Aluminum Aircraft Structure

PUBLISH DATE 2024
PAGES 23
SAE ARP4402 Rev A

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

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