Principal Engineer, Propulsion Integration

B.S., in Mechanical or Aerospace Engineering, or equivalent

8-12 years of experience in the design and development of propulsion systems

3+ years of direct experience with FADEC controlled turbofan engine integration in a Part 23 or Part 25 aircraft; familiarity with engine installation manuals

2+ years of involvement in bid, proposal, and project capture activities

Mastery of FAR Part 23 and Part 25 certification requirements and processes pertinent to the propulsion systems

Strong understanding and experience with RTCA D-160G, DO-178, DO-254, and SAE ARP4754A

Otto Aerospace provides a robust benefits package that includes competitive salaries, subsidized medical, dental, and vision coverage, 401(k) opportunities, paid short term disability, voluntary long-term disability and additional term life, with 15 paid days off, 13 paid holidays, and paid sick leave. Depending on seniority and role, some roles qualify for potential bonuses and stock options.

Otto Aerospace is an Equal Opportunity Employer

We are committed to diversity, equity, and inclusion in every aspect of our hiring process. All applicants will be considered for employment regardless of race, color, religion, sex, sexual orientation, gender identity, national origin, veteran status, or disability. We believe that a diverse team brings fresh perspectives, innovative ideas, and greater success. The more inclusive we are, the stronger we become. Applicants must be legally authorized to work in the U.S.

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Otto Aerospace is seeking a dynamic engineer to support and oversee the design, development, and integration of the propulsion system, including turbofan engines, FADECs, inlets, exhausts, heat exchangers, fans/blowers, and fire protection systems.

You will join a team developing the world’s most efficient aircraft.

Otto Aerospace is seeking first principles engineers that balance creativity with experience while working within an effective team atmosphere.

Perform 1-D analysis, as well as Computational Fluid Dynamics (CFD) analysis in support of aircraft subsystem integration, relating to fluid flow and heat transfer

Provide technical guidance for system owners in thermal science related activities, to include support with system level test planning, execution support, verification, data processing, and troubleshooting

Support development of engineering specifications and drawings