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A Comparison of the Capability of Sensitivity Level 3 and Sensitivity Level 4 Fluorescent Penetrants to Detect Fatigue Cracks in AluminumHistorically both sensitivity level 3 and sensitivity level 4 fluorescent penetrants have been used to perform NASA Standard Level inspections of aerospace hardware. In April 2008, NASA-STD-5009 established a requirement that only sensitivity level 4 penetrants were acceptable for inspections of NASA hardware. Having NASA contractors change existing processes or perform demonstration tests to certify sensitivity level 3 penetrants posed a potentially huge cost to the Agency. This study was conducted to directly compare the probability of detection sensitivity level 3 and level 4 penetrants using both Method A and Method D inspection processes. The study results strongly support the conclusion that sensitivity level 3 penetrants are acceptable for NASA Standard Level inspections
Document ID
20100015401
Acquisition Source
Goddard Space Flight Center
Document Type
Technical Memorandum (TM)
Authors
Parker, Bradford, H.
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Date Acquired
August 24, 2013
Publication Date
December 1, 2009
Subject Category
Quality Assurance And Reliability
Report/Patent Number
Rept-2010-00980
NASA/TM-2009-215850
Report Number: Rept-2010-00980
Report Number: NASA/TM-2009-215850
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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