SAE International Eddy Current Inspection of Open Fastener Holes in Aluminum Aircraft Structure ARP4402A

Description
This SAE Aerospace Recommended Practice establishes the requirements and procedures for eddy current inspection of open fastener holes in aluminum aircraft structures.
Description
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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Eddy Current Inspection of Open Fastener Holes in Aluminum Aircraft Structure - ARP4402A - SAE International
Warrendale, PA, United States
Eddy Current Inspection of Open Fastener Holes in Aluminum Aircraft Structure
ARP4402A
Eddy Current Inspection of Open Fastener Holes in Aluminum Aircraft Structure ARP4402A
This SAE Aerospace Recommended Practice establishes the requirements and procedures for eddy current inspection of open fastener holes in aluminum aircraft structures.

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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Technical Specifications

  SAE International
Product Category Standards and Technical Documents
Product Number ARP4402A
Product Name Eddy Current Inspection of Open Fastener Holes in Aluminum Aircraft Structure
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