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SAE ARP4402

Superseded

Superseded

A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.

View Superseded by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Superseded date

06-10-2020

Language(s)

English

Published date

11-06-2013

€114.14
Excluding VAT

1. SCOPE
2. APPLICABLE DOCUMENTS
3. TECHNICAL REQUIREMENTS
4. RESPONSIBILITY FOR INSPECTION
5. NOTES

Establishes the procedures and requirements for eddy current inspection of open fastener holes in aircraft structures.

DocumentType
Standard
Pages
16
PublisherName
SAE International
Status
Superseded
SupersededBy

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

NASA PRC 6509 : 2011 PROCESS SPECIFICATION FOR EDDY CURRENT INSPECTION
NASA STD 5005(INT) : 2007 THE DESIGN AND FABRICATION OF GROUND SUPPORT EQUIPMENT
NASA KSC DE 512-SM : 2012 FACILITY SYSTEMS, GROUND SUPPORT SYSTEMS, AND GROUND SUPPORT EQUIPMENT GENERAL DESIGN REQUIREMENTS
NASA STD 5009(INT) : 2006 NONDESTRUCTIVE EVALUATION REQUIREMENTS FOR FRACTURE CRITICAL METALLIC COMPONENTS
NASA STD 5009 : 2008 NONDESTRUCTIVE EVALUATION REQUIREMENTS FOR FRACTURE-CRITICAL METALLIC COMPONENTS - MEASUREMENT SYSTEM IDENTIFICATION: METRIC (INCH-POUND)

ASNT SNT TC 1A : 2016 TOPICAL OUTLINES FOR QUALIFICATION OF NONDESTRUCTIVE TESTING PERSONNEL
MIL-STD-410 Revision E:1991 NONDESTRUCTIVE TESTING PERSONNEL QUALIFICATION AND CERTIFICATION (EDDY CURRENT, LIQUID PENETRANT, MAGNETIC PARTICLE, RADIOGRAPHIC AND ULTRASONIC)

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