Senior Stress Engineer - Aircraft Structures

Bombardier

Colon (MI)

On-site

USD 50,000 - 67,000

Full time

3 days ago
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Benefits offered by this job

Insurance plans
Employee Assistance Program
Competitive base salary

Job summary

Bombardier in Mexico is seeking a Senior Specialist, Engineering, Stress to perform structural analysis on aircraft structures using FEM and hand methods, and to prepare substantiation reports.

You will work with cross-functional teams, review designs for load paths, and support certification activities with authorities such as FAA/EASA. The role requires 10+ years of stress engineering and proficiency in Patran/Nastran, CATIA V5, and strong English communication.

Qualifications

  • Bachelor of Engineering or equivalent required.
  • 10+ years of stress engineering experience.
  • Proficient in FEM tools and CAE software.
  • Experience with aircraft certification procedures.

Responsibilities

  • Perform structural analysis using hand methods and FEM on metallic and non-metallic structures.
  • Prepare formal engineering documentation (structural analysis reports, specs).
  • Present design review material for meetings with suppliers and internal/external customers.
  • Review designs for preliminary sizing of structural reinforcements and load path definitions.
  • Support design process from conceptual to detail design.
  • Write, review or approve substantiation reports for programs and certifying authorities (TCCA/FAA/EASA).
  • Assess primary and secondary structures from a static strength perspective.
  • Perform fatigue and damage tolerance assessments per mission profiles.
  • MRB duties in support of operations.

Skills

FEM tools
Microsoft Office
CATIA V5
Siemens NX
Aircraft certification
English proficiency
Independence
Load path analysis
MRB knowledge
Integration experience

Education

Bachelor of Engineering

Tools

Patran
Nastran
Nasgro
Altair
Hypermesh

Job description

Bombardier in Mexico is seeking a Senior Specialist, Engineering, Stress to perform structural analysis on aircraft structures using FEM and hand methods, and to prepare substantiation reports.

You will work with cross-functional teams, review designs for load paths, and support certification activities with authorities such as FAA/EASA. The role requires 10+ years of stress engineering and proficiency in Patran/Nastran, CATIA V5, and strong English communication.

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