our collaborators work together to evolve mobility around the world, one good idea after another. If you have a good idea, we have the environment to turn it into a unique product or an exceptional customer experience. Your ideas are our energy.
In your role, you will be required to:
Define structural integrity requirements for various system components such as landing gear, wheels & braking systems, FBW flight controls, high-lift flaps, hydraulic components, emergency power systems, fuel and inerting systems, pneumatic systems, engine and fire protection systems.
Develop structural integrity methodologies for said systems
Collaborate with suppliers, ensure compliance with methodology and program technical requirements.
Calculate and analyze loads.
Calculate and review static and fatigue analyses related to systems
Review supplier documents
Prepare certification reports.
As an ideal candidate,
You hold a Bachelor's degree in Mechanical or Aeronautical Engineering
You possess at least seven (7) years of experience with system load, stress, and fatigue analysis techniques
You are familiar with structural qualification requirements for aircraft systems, in particular: landing gear, "FBW" type electrical flight controls, hydraulic flight controls, horizontal stabilizer controls, high-lift flap controls, hydraulic and electro-mechanical components, conduits, etc.
You are familiar with landing gear load calculation methods
Knowledge of software such as CATIA, PATRAN is an asset.
Prior experience working on an aircraft development or in-service support program, including certification, would be an asset.
Experience as a delegate within a design approval organization (DAO) would be an asset.
You have a strong sense of responsibility, integrity, and are a team player
Good communication and computer skills are essential.
Details
- City
- Mirabel Southwest, Québec
Need help?
- support@aerowork.ca
- Phone
- 1-450-403-4300