Training

Structural Integrity & 
Fleet Life-Cycle Engineering Short Courses

Practical, instructor-led training for teams responsible for aircraft loads analysis, fatigue life assessment, and airworthiness oversight.

TDA short courses turn structural integrity science into engineering 
judgment that directly supports mission readiness.

who it’s for

who it’s for

  • Loads engineers
  • Stress and fatigue engineers
  • ASIP/structural integrity teams
  • Fleet life-cycle and usage analysts
  • Flight test and certification engineers
  • Program engineering leadership

FORMATS & Delivery

FORMATS & Delivery

  • On-site at your facility
  • Hosted at TDA offices
  • Private, program-specific sessions
  • Customization aligned to platform, mission profile, and data environment

Instructor Expertise

Instructor Expertise

Chance McColl, PhD
Loads, rotorcraft dynamics, gust analysis, aeroservoelasticity, flight dynamics

Chris Thaiss

Loads modeling, flight test procedures, certification support

Soonwook Kwon, PhD

Strength, fatigue, fracture mechanics, durability and damage tolerance

The appearance of U.S. Department of Defense (DoD) and industry visual information does not imply or constitute endorsement.

Explore the Course Offering

Aircraft External Loads


Course Length: 3 Days

Comprehensive overview of aircraft loads development, including maneuver, gust, buffet, ground, and landing impact; design/ultimate loads and repeated loads.

Covers:

  • Loads criteria and regulatory foundations
  • Time- and frequency-domain analysis
  • Aeroelastic considerations
  • Model development and validation
  • Practical, real-world problem solving

Outcome: Engineers understand how loads are generated, modeled, and validated for structural design.

Aircraft Gust Loads

Course Length: 3 Days

Advanced gust modeling for discrete and continuous turbulence environments.

Topics include:

  • Statistical foundations
  • Gust spectra development
  • Verification and validation
  • Application to fatigue testing
  • Integration into structural life analysis

Outcome: Clear understanding of gust-driven loading and its role in design and life-cycle modeling.

Loads for Non-Loads Engineers

Course Length: 2 Days

High-level overview of aircraft loads and how they influence structural decisions.

Designed for:

  • Stress, design, and flight test engineers
  • Program leadership
  • Cross-disciplinary teams

Outcome: Shared technical baseline across the program. Aircraft Structures: Loads, Strength, Durability & DADT Supports teams connecting loads and fatigue theory to fleet-level life-cycle oversight.

Aeroservoelasticity for Aircraft Loads Analysis

Course Length: 1.5–2 Days

Interaction of aerodynamic forces, structural flexibility, and control systems.

  • Aeroelastic coupling
  • Control system influence on loads
  • Loads reduction strategies
  • Modeling considerations

Outcome: Engineers understand how flight controls and structural dynamics influence final loads environments.

Ground Loads for Fixed & Rotary-Wing Aircraft

Course Length: 2 Days

Design criteria and analytical prediction of ground loads for shore-based and shipboard operations.

Covers:

  • Static and fatigue ground loads criteria
  • Dynamic model development
  • Certification considerations
  • Lessons learned from fleet programs

Rotary-Wing Aeromechanics

Course Length: 3 Days

Rotorcraft aerodynamics, structural dynamics, flight control, performance, and system design fundamentals.

Strength & Durability of Aircraft Structures

Course Length: 3-4 Days

In-depth exploration of fatigue behavior, fracture mechanics, 
and durability-based design.

Covers:

  • Crack initiation and crack growth modeling
  • Safe-life, fail-safe, total-life, and defect-tolerant methods
  • Coupon, component, and full-scale testing
  • Service loading analysis
  • Real-world case studies

Outcome: Engineers gain the physical and analytical foundation needed for defensible fatigue-life decisions.

Why Programs Invest in TDA Training

  • Establish a shared technical baseline
  • Improve life-cycle decision consistency
  • Reduce misinterpretation of loads and fatigue data
  • Strengthen ASIP and fleet life extension efforts