SAE ARP4402
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
View Superseded by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
Hardcopy , PDF
06-10-2020
English
11-06-2013
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Superseded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.
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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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