5+ years experience in primary metallic structure stress analysis
Advanced proficiency in nastran and patran software
Bachelor or master degree in mechanical or aeronautical engineering
The role involves ensuring that stress analysis for primary aircraft structures complies with certification requirements for static and fatigue conditions
Job Summary
The role involves ensuring that stress analysis for primary aircraft structures complies with certification requirements for static and fatigue conditions.
Candidates must possess at least five years of experience specifically analyzing primary metallic structures such as skins, frames, and stringers.
The position requires strong technical decision-making support regarding fixed and mobile supports while preparing key technical deliverables for Airbus Atlantic.
Matching Summary
The role involves ensuring that stress analysis for primary aircraft structures complies with certification requirements for static and fatigue conditions.
Skills & Requirements
Must-have
5+ years experience in primary metallic structure stress analysis
Advanced proficiency in NASTRAN and PATRAN software
Bachelor or Master degree in Mechanical or Aeronautical Engineering
Experience with Catia consultation and VBA programming
Knowledge of Airbus, Bombardier, and Airbus Canada calculation processes
Nice-to-have
Experience managing secondary structures and system installations
Project management experience
Strong written and oral communication skills
Ability to work autonomously and collaboratively in a team
Enthusiasm for fast-paced and unpredictable environments
Key Requirements
Minimum 5 years of primary structure stress analysis experience
Bachelor's or Master's degree in Mechanical or Aeronautical Engineering
Fluent English (technical) and French (verbal/meeting)