Heart Aerospace
Mechanical Design Engineer, Flight Mechanisms
Los Angeles, CAFrom $176kmidAdded today
About this role
Heart Aerospace seeks a Mechanical Design Engineer to develop flight control actuators, landing gear, and environmental systems for the ES-30 hybrid-electric regional aircraft. You'll own the design, analysis, fabrication, and certification of critical mechanisms while collaborating across electrical, software, and mechanical teams.
What you'll do
- Design, fabricate, and test novel flight control and propulsion components with full ownership from concept to certification
- Lead detailed design of subcomponents including gears, bearings, and seals for flight mechanisms
- Perform environmental qualification testing to aerospace standards such as DO-160G and MIL-STD-810
- Conduct FEA and hand-calculation analysis to validate mechanical designs
- Collaborate with cross-functional teams on electronic and software control system integration
- Support aircraft type certification efforts through design documentation and compliance
What they're looking for
- CAD software (NX, CATIA, SolidWorks, or equivalent)
- FEA analysis and hand-calculation methods for mechanical systems
- Pneumatic, hydraulic, and electromechanical system design
- Machine shop and manufacturing fundamentals with GD&T
- Aerospace design standards and regulatory compliance (DO-160G, FAA, EASA)
- Mechanical engineering fundamentals and component design
- Technical documentation and engineering drawings
- Cross-functional team collaboration
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Heart Aerospace
Heart Aerospace is developing the ES-30, a 30-passenger hybrid-electric regional aircraft, and is hiring engineers across propulsion, structures, software, and testing disciplines to design, integrate, and certify its innovative powertrain and airframe systems.
- Website
- heartaerospace.com
Likely interview questions
- Walk us through a flight mechanism or actuator system you designed—what were the critical design drivers and how did you validate them?
- Describe your experience with aerospace environmental qualification standards like DO-160G or MIL-STD-810. How have you applied them in design?