Building a Damage Findings Database using NLign Software Suite
Instructor: Mr Martin Raming - SwRI

Introduction to Structural Risk Assessment Theory and Applications Using the Smart|DT Software
Instructor: Dr Harry Millwater - University of Texas at San Antonio

End-to-End Case Study: Computation of Fracture Mechanics Parameters (KI, KII, and KIII) for Complex 3D Aerospace Parts Using StressCheck v12.1
Instructor: Mr Brent Lancaster - ESRD Inc

Practical Risk Analysis Using PROF
Instructor: Ms Laura Hunt - SwRI

Fatigue Loads and Damage Tolerance Methods for Airworthiness
Instructor: Mr James Burd - Aeronautica LLC

Aircraft Composite Inspection – Improving the Manual Inspection Process with Modern Scanning Techniques
Poster Presenter: Mr Jeffrey Register - Evident Scientific

Traditional Aircraft Ultrasonic inspection versus Phased Array – How Phased Array Techniques Improve Inspection Reliability and Reduce Program Costs
Poster Presenter: Mr Jeffrey Register - Evident Scientific

Failure Analysis of T38 Stators from the Brake Assembly
Poster Presenter: Ms Mirella Vargas - SwRI

Electrochemical InSitu Treatment of Fatigue Cracks in Aircraft Metals Using the Grapheno1 System
Poster Presenter: Dr Konstantin Dolgan - Grapheno LLC

Disbond Damage Detection Capabilities of a Piezo Sensor based SHM System in a CompositeMetallic Step Lap Joint
Poster Presenter: Mr Marco Schnidrig - HSLU TA

Eliminating Life Extension Modifications Through FEA CI and DTA of a Historically SafeLife Managed Aircraft
Poster Presenter: Mr Nicholas Hatcher - Andromeda Systems Inc

Utilizing Fiber Reinforced Aluminum for Structural and Repair Applications
Poster Presenter: Mr Brandon Coates - Touchstone Research Lab

Innovation in Aerospace Eddy Current NDT
Poster Presenter: Mr John Hansen - ETher NDE Ltd

Toward a Low Swap Conformal Corrosion Health Monitoring System for Structural Integrity and Lifecycle Extension Programs
Poster Presenter: Dr John Williams - The Boeing Co

Welcome/ASIP Manager of the Year/Lincoln Award

US Navy F/A-18 E/F Super Hornet's Successful SLAP/SLEP Implementation
Presenter: Mr Russell Bruns - NAWC Patuxent River

UK RAF Approach to H-47 Structural Integrity
Presenter: Mr Michael Kachmar - The Boeing Co

E-7A Wedgetail Royal Australian Air Force: Inservice Calibration of the E-7A AEWC Wedgetail Operational Loads Monitoring System
Presenter: Mr David Craze - Boeing Defence Australia

Luncheon Presentation
Luncheon Speaker: Ms Lily Arcusa - AFLCMC

Jayhawk Integrity: ASIP Refresh & Lessons Learned on the T-1A
Presenter: Mr Ryan Melcher - Textron Aviation Defense

Characterising Small and Near-threshold Fatigue Crack Growth Rates in Aircraft Aluminium Alloys Using Quantitative Fractography for ASIP Tasks
Presenter: Dr Ben Main - Defence Science Technology Group DSTG

A Modified Random Forest Approach for Fatigue Spectrum Reduction in Aircraft Structures
Presenter: Mr Moises Ocasio - The Boeing Co

Addressing Industry Need for a Rapid Fatigue Method for Airframe Analysis and Sizing
Presenter: Mr Aleksandr Breit - Collier Aerospace

Tailoring Airworthiness Requirements to Legacy Modification Programs
Presenter: Mr Joshua Lichti - The Boeing Co

T-7A Windshield and Canopy Bird Strike - Analysis, Redesign and Certification
Presenter: Mrs Leah Lenzner - The Boeing Co

How Much Inspection Is Enough
Presenter: Mr Travis Reese - USAF/OC-ALC

F-16 Usage Data Collection and Evaluation – A Brief History, Field Challenges and Overcoming Obstacles
Presenter: Mr James O'Connor - Leidos

T-38 NCheck Fleet Use for ACIs and Paint Scoring
Presenter: Mr Matthew Andrus - USAF

Preparing For “Above 100”
Presenter: Dr Albert Arrieta - Lockheed Martin Co

C-130 ESL Wing Durability Test Turning Challenges into Opportunities
Presenter: Dr Albert Arrieta - Lockheed Martin Co

T-7A Truncation Testing Trials and Tribulations
Presenter: Mr Jason Hawks - The Boeing Co

Witness Integrity Sensor Platform-A Companion Tool for Digital Twin Models
Presenter: Dr Seth Kessler - Metis Design Corp

EIDS Needs: How NDI Material Variability and Limited Data Can Affect Risk Analysis
Presenter: Ms Laura Hunt - SwRI

Effects of Edge Margin on Fatigue and Crack Growth Life at SsCx Holes in 7050-T7451 Plate
Presenter: Mr James Prather - Lockheed Martin Co

A Method to Combine Maneuver and Relevant Buffet Loads in Time Domain to Generate Fatigue Design Spectra and Allowables Relative to Design to Global FEM
Presenter: Mr Jason Kath - The Boeing Co

T-7A Overview and Lessons Learned from Flight Loads and Flutter Testing
Presenter: Mr Eric Primm - The Boeing Co

Establishment of Operational Fatigue Spectra for the C-5 Landing Gears
Presenter: Dr John Hollkamp - UDRI

Supplemental Test Program for EIDS Development
Presenter: Dr Emiel Amsterdam - Royal Netherlands Aerospace Centre NLR

Damage Tolerance of Interference-Fit Fasteners under Fatigue Loading
Presenter: Dr Marcus Stanfield - SwRI

Experience of Baseline Operational Spectrum (BOS) for the F-35A Fleet and Usefulness for Fleet Management
Presenter: Mr David Mauldin - Lockheed Martin Co

Integrating Corrosion Modeling with Digital Engineering
Presenter: Dr Kristen Williams - The Boeing Co

Cold Spray Technology Resets the Corrosion Clock on Metallic Parts
Presenter: Dr Bruno Zamorano Senderos - The Boeing Co

Hydrogen Environmentally Assisted Cracking (HEAC) of Some 7XXX Aluminum Alloys
Presenter: Ms Dana Rosenbladt - The Boeing Co

Damage Tolerance and Inspection Considerations for Certification of Metal AM Parts in Aviation
Presenter: Dr Michael Gorelik - FAA

Advancements Towards Analytical Damage Tolerance Assessments of Composite Structures
Presenter: Dr Brian Justusson - The Boeing Co

Predicting the Effects of Damping Tape for Acoustic Analysis
Presenter: Mr Dylan Kindred - USAF

Development and Execution of a Bolt Hole Eddy Current Probability of Detection (PoD) Capability Study within 7050-T7451 Aluminum
Presenter: Mr Adam Barrett - USAF AFRL/RX

Nondestructive Evaluation for Engineered Residual Stress Assessment
Presenter: Dr Eric Lindgren - USAF AFRL/RX

Development of Validation Data Through Quantitative Fractography (QF) for Improved Crack Growth Analysis
Presenter: Dr Scott Carlson - Lockheed Martin Aeronautics