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SAE ARP4402A : 2020 (2024)

Eddy Current Inspection of Open Fastener Holes in Aluminum Aircraft Structure

Standard Details

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

Cross Reference: ATA105,MIL-STD-410,SNT-TC-1A

General Information

Status : Reaffirmed
Standard Type: Main
Document No: SAE ARP4402A : 2020 (2024)
Document Year: 2024
Pages: 23

Life Cycle

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Reaffirmed
SAE ARP4402A : 2020 (2024)
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