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SAE ARP 4402 A : 2020

Superseded

Superseded

A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.

View Superseded by

Eddy Current Inspection of Open Fastener Holes in Aluminum Aircraft Structure

Available format(s)

Hardcopy , PDF

Superseded date

25-09-2024

Superseded by

SAE ARP4402A:2020(R2024)

Language(s)

English

Published date

22-09-2020

€129.21
Excluding VAT

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
Superseded
SupersededBy
Supersedes

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

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