risk analysis

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Southwest Research Institute® (SwRI®) structural engineering specialists use probabi- listic 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 evalu- ate alternative usage, maintenance and inspec- tion 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. Aircraft Risk Analysis D015763 KEYWORDS Risk Assessment Probability of Fracture Fatigue Fracture Failure Damage Tolerance Inspection Interval PROF POD EIFS Crack Growth Aircraft Usage Random Variables Sensitivity Studies Economic Life Hazard Rate MIL-STD-882D JSSG-2006 Training/Short Course Southwest Research Institute ® D015764 Single-flight probability of failure (SFPOF) results with and without recurring inspections 0 1,000 2,000 3,000 4,000 5,000 Initial Inspection at 4.250 hrs Recurring Inspection at 1,500 hrs Flight Hours SFPOF 6,000 7,000 8,000 9,000 10,000 With Recurring Inspections at 1,500 hrs Without Inspections Capabilities n Risk evaluations of in-service cracking n Evaluation of safety and economic impacts of service life extensions n Risk-based evaluations of inspection, repair and/or modification plans n Single aircraft and fleet-wide risk analyses n Development of random variable proba- bilistic distributions for risk analyses n Probabilistic fatigue and fracture analyses n Equivalent Initial Flaw Size (EIFS) distribution development using in-service cracking and teardown data n Probability of Detection (POD) curve development for nondestructive inspection method n Interpretation of risk analysis results in terms of MIL-STD-882D and JSSG-2006 n Economic life evaluations n Sensitivity studies n Risk assessment workshops and training SwRI performs risk analyses of in-service cracking detected in aircraft structures

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Risk Analysis of aircraft

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  • Southwest Research Institute (SwRI) structural engineering specialists use probabi-listic 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 evalu-ate alternative usage, maintenance and inspec-tion 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 SwRIs 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.

    Aircraft Risk Analysis

    D015

    763

    KEYWORDS

    Risk Assessment

    Probability of Fracture

    Fatigue

    Fracture

    Failure

    Damage Tolerance

    Inspection Interval

    PROF

    POD

    EIFS

    Crack Growth

    Aircraft Usage

    Random Variables

    Sensitivity Studies

    Economic Life

    Hazard Rate

    MIL-STD-882D

    JSSG-2006

    Training/Short Course

    SouthwestResearchInstitute

    D015

    764

    Single-flight probability of failure (SFPOF) results with and without recurring inspections

    0 1,000 2,000 3,000 4,000 5,000

    Initial Inspection at 4.250 hrsRecurring Inspection at 1,500 hrs

    Flight Hours

    SFPO

    F

    6,000 7,000 8,000 9,000 10,000

    With Recurring Inspections at 1,500 hrs

    Without Inspections

    Capabilities n Risk evaluations of in-service cracking

    n Evaluation of safety and economic impacts of service life extensions

    n Risk-based evaluations of inspection, repair and/or modification plans

    n Single aircraft and fleet-wide risk analyses

    n Development of random variable proba- bilistic distributions for risk analyses

    n Probabilistic fatigue and fracture analyses

    n Equivalent Initial Flaw Size (EIFS) distribution development using in-service cracking and teardown data

    n Probability of Detection (POD) curve development for nondestructive inspection method

    n Interpretation of risk analysis results in terms of MIL-STD-882D and JSSG-2006

    n Economic life evaluations

    n Sensitivity studies

    n Risk assessment workshops and training

    SwRI performs risk analyses of in-service cracking detected in aircraft structures

  • Southwest Research Institute is an independent, nonprofit, applied engineering and physical sciences research and development organi-zation using multidisciplinary approaches to problem solving. The Institute occupies 1,200 acres in San Antonio, Texas, and provides more than 2 million square feet of laboratories, test facilities, work-shops and offices for more than 3,100 employees who perform contract work for industry and government clients.

    Benefiting government, industry and the public

    through innovative science and technology

    Joseph W. Cardinal, P.E., Staff EngineerStructural Integrity Analysis(210) [email protected]

    Structural Engineering DepartmentMechanical Engineering DivisionSouthwest Research Institute6220 Culebra Road (78238-5166)P.O. Drawer 28510 (78228-0510)San Antonio, Texas

    www.swri.orgwww.structural-engr.swri.orgAn Equal Opportunity Employer M/F/D/V

    Committed to Diversity in the Workplace

    18-0

    411

    JCN

    2406

    12 b

    l

    We welcome your inquiries.

    For additional information, please contact:

    SFPOF for recurring inspections and different detectable flaw sizes

    1,0001.E-15

    1.E-14

    1.E-13

    1.E-12

    1.E-11

    1.E-10

    1.E-09

    1.E-08

    1.E-07

    1.E-06

    1.E-05

    1,200 1,400 1,600 1,800

    Flight Hours (IFF)

    SFPO

    F

    2,000 2,200 2,400

    Median Defectable = 0.05 inchesMedian Defectable = 0.10 inchesMedian Defectable = 0.15 inches

    Experience n Damage Tolerance Risk Assessment of T-38 Wing Skin Cracks n Risk Assessment of T-37B Fatigue Critical Locations

    n Risk Assessment of the A-10 Wing Aft Lower Cover at Rear Spar Cap (WS 23)

    n Risk and Economic Implications of DADTA for F-5 Foreign Operators

    n Probabilistic Structural Analyses of Fatigue and Fracture

    n Advanced Probabilistic Fracture Mechanics and Life Evaluations of Turbine Rotor Blade Attachments

    Analysis Tools for Risk Assessment

    n PROF

    n DARWIN

    n NESSUS

    n Weibull Analyses

    D015

    765