SAE ARP4402A

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Eddy Current Inspection of Open Fastener Holes in Aluminum Aircraft Structure

Published by Publication Date Number of Pages
SAE 2024 23

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

SAE ARP4402A establishes the requirements and procedures for eddy current inspection of open fastener holes in aluminum aircraft structures.

Product Details

Published:
09/17/2024
Number of Pages:
23
File Size:
1 file 520 KB
Note:
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