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SAE ARP 4402 A : 2020

Current

Current

The latest, up-to-date edition.

Eddy Current Inspection of Open Fastener Holes in Aluminum Aircraft Structure

Available format(s)

Hardcopy , PDF

Language(s)

English

Published date

09-22-2020

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

Committee
AMS K
DocumentType
Revision
Pages
23
PublisherName
SAE International
Status
Current
Supersedes

NASA-STD-5009C:2023 Nondestructive Evaluation Requirements for Fracture Critical Metallic Components

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US$141.60
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