Airframe Design Engineer

Electra•Manassas, VA

1d•$92,000 - $112,000•Onsite

About The Position

Electra is seeking an Airframe Design Engineer to help with the design, integration, and development of primary and secondary structures for their nine-passenger EL9 hybrid-electric aircraft. In this role, you will support major structural design deliverables, collaborate deeply with multidisciplinary teams, and help ensure the aircraft's structures meet performance, safety, manufacturability, and certification goals. This position is ideal for an experienced engineer ready to contribute at a high level while influencing design decisions across multiple aircraft systems. This role is based at our Manassas, VA headquarters, with on-site presence strongly preferred, and includes occasional travel (under 10%).

Requirements

Bachelor's degree in Aerospace Engineering, Mechanical Engineering, or related field; Master's degree preferred
2+ years of experience in aircraft structural or airframe design, integration, and development (or equivalent combination of education and experience)
Strong understanding of airframe structural design for both metallic and composite components
Demonstrated experience across conceptual, preliminary, and detailed design phases
Proficiency with 3D CAD tools (preferably Siemens NX or CATIA V5/V6)
Familiarity with FAA Part 23 or Part 25 structural certification requirements
Working knowledge of loads, stress, and fatigue principles and their influence on design decisions
Experience creating aerospace engineering drawings, design documentation, and configuration-controlled deliverables
Strong communication and collaboration skills for effective cross-functional teamwork
Ability to manage design tasks, priorities, and deadlines in a fast-paced development environment

Nice To Haves

Experience with hybrid-electric, eSTOL/eVTOL, or other advanced aircraft development programs
Familiarity with composite manufacturing processes such as AFP, infusion, or hand layup
Experience with FEM tools (NASTRAN, FEMAP, HyperMesh)
Background in weight optimization, design-for-manufacturability, or design-to-cost
Knowledge of requirements management or PLM tools (JAMA, Teamcenter, etc.)
Experience coordinating with suppliers on design, fabrication, or integration activities
Private pilot license or a strong passion for aviation

Responsibilities

Support the design and development of primary and secondary airframe structures, including fuselage, wing, empennage, and landing gear integration.
Assist with structural design tasks from concept through detailed design and into certification, ensuring compliance with performance, manufacturability, maintainability, and safety requirements.
Work with structural requirements, material selections, and design criteria in support of applicable airworthiness regulations.
Collaborate with aerodynamics, propulsion, systems, manufacturing, stress, and certification teams to ensure integrated and optimized structural solutions.
Produce high-quality design documentation, including 3D CAD models, engineering drawings, ICDs, and supporting design reports.
Execute trade studies evaluating materials, configurations, manufacturing approaches, and integration options to balance weight, cost, and performance.
Support structural analysis activities by working closely with stress engineers on static, dynamic, and fatigue considerations.
Participate in design reviews and provide technical mentorship to early-career engineers.
Work with suppliers on manufacturability, design-for-production, and technical issue resolution.
Contribute to continuous improvement in Electra's structural design methods, tools, and development processes.
Stay informed on emerging technologies, advanced materials, and evolving FAA certification requirements for new aircraft types.
Support CAD admin duties such as tool and process development for designers.