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A Methodology to Evaluate the Feasibility of Descoping Nondestructive Evaluation (NDE) Fracture Control Requirements in NASA-STD-5019AA new methodology is proposed to evaluate the risk of structural failure if NDE flaw screening requirements are relaxed, which is referred to as an NDE descope. The proposed method estimates the probability of a critical initial flaw size (CIFS) existing in a part based on a historical record of NDE inspections that are predictive of flaw existence in future parts fabricated under the same time-invariant process control. The methodology conservatively assumes that the CIFS is equal to the NDE detectable flaw size, and it further assumes that if a CIFS defect exists it will lead to structural failure during the part’s operational lifetime. While conservative, these assumptions are necessary to utilize historical NDE databases that do not include flaw size characterization.

The proposed risk evaluation method is based on the premise that if the probability of CIFS defect existence is considered sufficiently low, leading to an acceptably low risk of primary structural failure, then rationale for descoping NDE may exist. Acceptable risk of structural failure is application/system specific. Descoping NDE is shown to result in an elevated risk acceptance posture even if a sufficiently large NDE database is available and there are no flaw detections in the inspection history. The method depends on time-invariant process control and assumes that the part was initially damage tolerant prior to descope.
Document ID
20250004074
Acquisition Source
Langley Research Center
Document Type
Technical Memorandum (TM)
Authors
Patrick E. Leser
(Langley Research Center Hampton, United States)
Peter A. Parker
(Langley Research Center Hampton, United States)
William H. Prosser
(Langley Research Center Hampton, United States)
Bence B. Bartha
(Kennedy Space Center Merritt Island, Florida, United States)
K. Elliott Cramer
(Langley Research Center Hampton, United States)
Date Acquired
April 23, 2025
Publication Date
April 1, 2025
Publication Information
Publisher: National Aeronautics and Space Administration
Subject Category
Space Transportation and Safety
Statistics and Probability
Report/Patent Number
TI-23-01904
NASA/TM-20250004074
NESC-RP-23-01904
Funding Number(s)
WBS: 869021.01.23.01.01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Technical Review
NASA Peer Committee
Keywords
Risk Evaluation
Fracture-Critical Components
Nondestructive Evaluation
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