Senior Fatigue & Damage Tolerance Engineer

Airbus

Wichita (KS)

On-site

USD 120,000 - 160,000

Full time

6 days ago
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Benefits offered by this job

Competitive base salary
Profit sharing / ESOP
Paid time off
Comprehensive insurance
Leadership University

Job summary

Airbus Americas, Inc. in Wichita, KS is seeking a Fatigue & Damage Tolerance Engineer to support aerospace structure analysis.

The role involves performing complex FDT analyses using both hand calculations and computer techniques, collaborating with design and static stress teams to develop high strength-to-weight structures. The ideal candidate has 7+ years of airframe analysis experience, with proficiency in classical and FEM methods, and strong English communication skills.

Qualifications

  • 7+ years total experience in analysis with airframe structures, including fatigue and/or damage tolerance.
  • In-depth knowledge of classical and numerical (Finite Element) stress analysis methods.
  • Capable of working in a dynamic, fast-paced environment both independently and collectively.

Responsibilities

  • Autonomously perform complex durability and damage tolerance analyses to verify structural integrity.
  • Document analyses in support of trade studies or detail drawing sign-off for airframe structure.
  • Liaise with Design, Static Stress and other Airbus departments to develop optimum design solutions.
  • Lead in the preparation of complex business and technical material and presentation packages.
  • Mentor and provide leadership to less experienced structural analysts.

Skills

Fatigue & Damage Tolerance analysis
Airframe structural analysis
Finite Element analysis
English communication

Education

Bachelor of Science in Engineering

Tools

NASTRAN
PATRAN
CATIA
MS Excel
Google Suite

Job description

Airbus Americas, Inc. in Wichita, KS is seeking a Fatigue & Damage Tolerance Engineer to support aerospace structure analysis.

The role involves performing complex FDT analyses using both hand calculations and computer techniques, collaborating with design and static stress teams to develop high strength-to-weight structures. The ideal candidate has 7+ years of airframe analysis experience, with proficiency in classical and FEM methods, and strong English communication skills.

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