EDDY CURRENT INSPECTION OF OPEN FASTENER HOLES IN ALUMINUM AIRCRAFT STRUCTURE

Available format(s)

Hardcopy , PDF

Superseded date

10-06-2020

Language(s)

English

Published date

06-11-2013

Publisher

SAE International

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.

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)

US$125.08

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Abstract