| Location | Manassas, VA |
| Salary | $130,000–$180,000 Per Year |
About Electra
At Electra, we''re building hybrid-electric Ultra Short Takeoff and Landing aircraft that redefine regional air travel. Our technology enables aircraft to take off and land in soccer field-sized spaces, unlocking thousands of new operating locations and enabling what we call Direct Aviation: quiet, efficient, point-to-point travel closer to where people live and work.
A global company headquartered in Manassas, VA, with additional operations in Switzerland, Electra is backed by industry leaders and is advancing toward certification. We''re a growing team of innovators working at the forefront of sustainable aviation-every hire plays a critical role in shaping the future of flight.
The Role
As a Senior or Principal Airframe Stress Engineer, you will lead structural analysis efforts supporting the development, certification, and production of Electra''s flagship hybrid-electric eSTOL aircraft. This role is responsible for ensuring the structural integrity of metallic and composite airframe components through detailed analysis, testing, and certification substantiation.
You will work closely with design engineering, loads, materials & processes, manufacturing, structural test, suppliers, and certification teams to develop robust airframe structures that meet performance, safety, and FAA certification requirements. The ideal candidate combines deep structural analysis expertise with strong engineering judgment and the ability to influence aircraft design decisions throughout the product lifecycle.
What You''ll Do
Support development of major airframe structures from preliminary design through certification, production launch, and manufacturing ramp-up
Perform static strength, fatigue, and durability analyses for metallic and composite aircraft structures
Develop structural substantiation methods and analysis plans supporting FAA Part 23 type certification
Create and validate finite element models using FEMAP/Nastran or equivalent analysis tools
Perform detailed hand calculations using industry-standard methodologies and references including:
Bruhn
Niu
Roark
ESDU
Classical mechanics of materials approaches
Collaborate with loads, design, materials & processes, manufacturing, structural test, and certification teams throughout the entire development process
Support trade studies and structural design optimization activities
Define structural analysis requirements and certification substantiation plans
Review and approve design dispositions and engineering analyses
Support component, subassembly, and full-scale structural testing activities, including:
Test planning
Requirements definition
Instrumentation support
Data review
Test reporting
Prepare structural substantiation reports and certification documentation
Present structural analyses and recommendations during internal and external design reviews
Support supplier technical reviews and provide guidance on structural analysis methodologies
Contribute to the establishment of structural analysis processes, best practices, and design standards
What You''ll Bring
Bachelor''s degree in Aerospace Engineering, Mechanical Engineering, or related engineering discipline
Experience in airframe structural analysis supporting aircraft development programs
Strong knowledge of metallic and composite aircraft structures
Experience supporting FAA Part 23 and/or Part 25 aircraft certification programs
Advanced proficiency with FEMAP/Nastran or equivalent finite element analysis tools
Experience with NX or similar CAD platforms
Strong understanding of:
Aircraft loads
Free body diagrams
Structural load paths
Mechanics of materials
Structural stability and failure modes
Advanced proficiency performing both hand calculations and finite element analyses
Experience developing structural substantiation reports and certification documentation
Strong technical writing and communication skills
Ability to work effectively within multidisciplinary engineering teams
Strong analytical and problem-solving capabilities
Preferred Qualifications
Location & Travel
Location: Manassas, VA Headquarters. This position requires regular onsite presence to support collaboration with engineering, manufacturing, and test teams.
Travel: Minimal
Leveling Expectations
Level (Senior or Principal) will be determined based on the candidate''s experience, technical expertise, demonstrated leadership, and ability to influence aircraft development decisions.
Both levels require expertise in aircraft structural analysis, certification substantiation, and aircraft development. Differentiation is based on technical leadership, scope of responsibility, independence, and organizational influence.
Senior Airframe Stress Engineer (8+ Years)
Principal Airframe Stress Engineer (10+ Years)
Compensation
$130,000.00 - $180,000.00 annually. This range reflects the anticipated hiring range across all eligible locations; actual compensation is determined based on relevant experience, education, skills, level, and geographic location. Total compensation includes performance bonus, equity eligibility, and comprehensive benefits.
What We Offer