Analyze composite & hybrid structures for static strength according to validated methods.
Ensure adherence to airworthiness regulations, relevant design principles, processes, methods and manufacturing capabilities guidelines.
Define, interpret and validate tests.
Interface and communicate with relevant stakeholders.
Provide relevant input to design for the creation of drawings for manufacture and support to other functions (i.e. production, customer support) as needed.
Provide stress analysis for the repair/acceptance of damaged structures.
Perform monitoring/guidance/support of Sub-contracting firms providing structure analysis work.
As our ideal candidate,
You hold a Bachelor's degree in Mechanical or Aeronautical Engineering
You have a minimum of seven (7) years in stress analyses pertaining to composite and metallic components
Experience on A220 Structures is an asset
Knowledge of NASTRAN, PATRAN, CATIA V5, and MS Office is required
Knowledge of ADAMS and the Google Suite is an asset
Previous work on an aircraft development or in-service programs including certification is an asset
You ideally have delegation experience in a Design Aircraft Organization
You possess a strong sense of responsibility and integrity, you are self-motivated and team player.
You have good oral/written communication skills in french and in english
Oral/written communication skills and computer skills are essential.