Aircraft Risk Analysis

Southwest Research Institute® (SwRI®) structural engineering specialists use
probabilistic methods to perform risk assessments to quantify the safety and
useful service life of aircraft structures in terms of probability of failure
and hazard rate. These analyses evaluate alternative usage, maintenance, and
inspection scenarios in terms of safety-of-flight risk and can be used to make
planning decisions by balancing safety, cost and readiness of the aircraft
system.
SwRI engineers use analysis tools such as the USAF probability of fracture
(PROF) software and other advanced probabilistic methods contained in SwRI’s
NESSUS® and DARWIN® software to assess the effects of variabilities and
uncertainties in loadings, material properties, fatigue and fracture models,
flaw sizes, and inspection methods on the risk of structural failure.
Capabilities
- Risk evaluations of in-service cracking
- Evaluation of safety and economic impacts of service life extensions
- Risk-based evaluations of inspection, repair and/or modification plans
- Single aircraft and fleet-wide risk analyses
- Development of random variable probabilistic distributions for risk
analyses
- Probabilistic fatigue and fracture analyses
- Equivalent Initial Flaw Size (EIFS) distribution development using
in-service cracking and teardown data
- Probability of Detection (POD) curve development for nondestructive
inspection methods
- Interpretation of risk analysis results in terms of MIL-STD-882D and
JSSG-2006
- Economic life evaluations
- Sensitivity studies
- Risk assessment workshops and training
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Single-flight probability of failure (SFPOF) results
with and without recurring inspections
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Experience
- Damage Tolerance Risk Assessment of T-38 Wing Skin Cracks
- Risk Assessment of T-37B Fatigue Critical Locations
- Risk Assessment of the A-10 Wing Aft Lower Cover at Rear Spar Cap (WS
23)
- Risk and Economic Implications of DADTA for F-5 Foreign Operators
- Probabilistic Structural Analyses of Fatigue and Fracture
- Advanced Probabilistic Fracture Mechanics & Life Evaluations of Turbine
Rotor Blade Attachments
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SwRI performs risk analyses of in-service cracking
detected in aircraft structures
|
Analysis Tools for Risk Assessment
- PROF
- DARWIN®
- NESSUS®
- Weibull Analyses
SFPOF for recurring inspections and different
detectable flaw sizes
|
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This flyer was published in September 2007. For more information about
Aircraft Risk Analysis, contact
Joseph W. Cardinal, Staff Engineer, Phone (210) 522-3323, Fax (210)
522-3042,
Mechanical Engineering Division, Southwest
Research Institute, P.O. Drawer 28510, San Antonio, Texas 78228-0510.
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