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  April 8, 2008  
  Presented and demonstrated at ASNT Colorado Chapter. Title of presentation: “Thick & Multi-Layer Aircraft Structure NDI Using Remote Field Eddy Current (RFEC) Technique”.  
  March 24-26, 2008  
  1. Presented and demonstrated at 2008 NDT Symposium sponsored by Lockheed Martin.
    1. Titles of presentations:
      1. FG RFEC technique for through bushing bolt hole inspection;
      2. FG RFEC technique for thick multilayer aircraft structure inspection.
    1. Topics of demonstrations:
      • Through composite inspection;
      • Boeing 707 wing structure inspection;
      • C-130 wing structure inspection;
      • Through bushing inspection (1);
      • Through bushing inspection (2);
      • Corrosion detection in thick multilayer structure.
 
  February 5, 2008.  
  Starting SBIR Phase II Extension entitled “Development of remote field eddy current NDI technique for nondestructive inspection (NDI) of fastener hole in thick multi-layer structure”.  
  December 4-7, 2007  
  Post presentation at ASIP Conference 2007, Palm Spring, CA. Title “Inspection of Fastener Hole Cracks Using Motorized Remote Field Eddy Current Probe”.  
  November 28-29, 2007  
  Attended by invitation the Commercialization Pilot Program (CPP) and JSF/F-22 SBIR Transition Workshop at Ft. Worth, TX. Interview by Boeing & Lockheed Martin.  
  August 30, 2007  
  Successful completion of SBIR Phase II project entitled “Development of remote field eddy current NDI technique for nondestructive inspection (NDI) of fastener hole in thick multi-layer structure”.  
  August 28, 2007  
  Successful demonstration of through bushing inspection scanner at Hill AFB  
  July 23 - July 27, 2007
  Presentation at 34th Annual Review of Progress in QNDE, Golden, CO. Title “Applications of Motorized Rotational RFEC Probes in Thick and Multilayer Structure Crack Detection”.

 

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