Pivotal
Verification Engineer - Aeromechanical (Design & Test)
About this role
Pivotal seeks a Verification Engineer for its Aeromechanical team, focusing on verification activities for aeromechanical subsystems of electric Vertical Takeoff and Landing (eVTOL) aircraft. This role involves managing end-to-end processes from design to testing, playing a key role in ensuring aircraft performance and safety.
What you'll do
- Own verification activities for aeromechanical subsystems
- Manage requirements through design to test execution
- Conduct test planning and reporting
- Work across design and physical testing environments
- Ensure performance, safety, and reliability of the aircraft
- Collaborate with cross-functional teams
What they're looking for
- Experience in verification engineering
- Understanding of aeromechanical systems
- Test planning and execution skills
- Strong analytical and problem-solving abilities
- Cross-functional collaboration
- Knowledge of safety and reliability standards
- Attention to detail
- Effective communication skills
Benefits
- Opportunity to work in an emerging technology field
- Dynamic and hands-on team environment
- Growth potential with the company
- Engagement in innovative aircraft design
- Work on projects with real-world applications
- Contribute to the future of mobility
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Pivotal
Pivotal develops innovative electric Vertical Takeoff and Landing (eVTOL) aircraft, including models like BlackFly and Helix, with a focus on aeromechanical systems, flight control, and autonomous capabilities. The company is hiring verification engineers, quality engineers, motor controls engineers, firmware engineers, and computer vision engineers to advance aircraft performance, safety, manufacturing quality, and autonomous perception systems.
View all jobs at PivotalLikely interview questions
- Walk us through your experience with end-to-end verification workflows—from requirements through test planning, execution, and reporting. What tools or methodologies did you use?
- Describe a time you had to verify a complex aeromechanical subsystem. What challenges did you encounter and how did you solve them?