SAE ARP4402A-2020 (2024) Reaffirmed

Eddy Current Inspection of Open Fastener Holes in Aluminum Aircraft Structure

标准摘要

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
英文名称Eddy Current Inspection of Open Fastener Holes in Aluminum Aircraft Structure

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