NASA PRC 6509 : 2011
Withdrawn
A Withdrawn Standard is one, which is removed from sale, and its unique number can no longer be used. The Standard can be withdrawn and not replaced, or it can be withdrawn and replaced by a Standard with a different number.
PROCESS SPECIFICATION FOR EDDY CURRENT INSPECTION
29-06-2011
29-06-2011
1.0 SCOPE
2.0 APPLICABILITY
3.0 USAGE
4.0 REFERENCES
5.0 PROCESS REQUIREMENTS
6.0 SPECIAL NDE QUALIFICATION
7.0 DEVIATIONS AND WAIVERS
8.0 TRAINING AND CERTIFICATION OF PERSONNEL
9.0 DEFINITIONS
Sets up the minimum requirements for eddy current inspection of flat surfaces, fastener holes, threaded fasteners and seamless and welded tubular products made from nonmagnetic alloys such as
| DocumentType |
Standard
|
| PublisherName |
National Aeronautics and Space Administration
|
| Status |
Withdrawn
|
| NASA STD 5019 : 2016 | FRACTURE CONTROL REQUIREMENTS FOR SPACEFLIGHT HARDWARE |
| NASA PRC 5010 : 2007 | PROCESS SPECIFICATION FOR PICKLING, ETCHING, AND DESCALING OF METALS |
| SAE AS4787 | Eddy Current Inspection of Circular Holes in Nonferrous Metallic Aircraft Engine Hardware |
| NAS410:2003 | NAS CERTIFICATION & QUALIFICATION OF NONDESTRUCTIVE TEST PERSONNEL |
| NASA STD 5019 : 2016 | FRACTURE CONTROL REQUIREMENTS FOR SPACEFLIGHT HARDWARE |
| ASTM E 426 : 2016 : REDLINE | Standard Practice for Electromagnetic (Eddy Current) Examination of Seamless and Welded Tubular Products, Titanium, Austenitic Stainless Steel and Similar Alloys |
| NASA STD 5009 : 2008 | NONDESTRUCTIVE EVALUATION REQUIREMENTS FOR FRACTURE-CRITICAL METALLIC COMPONENTS - MEASUREMENT SYSTEM IDENTIFICATION: METRIC (INCH-POUND) |
| SAE ARP4402 | Eddy Current Inspection of Open Fastener Holes in Aluminum Aircraft Structure |
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