Evaluate the strength and integrity of structural non-conformances and repairs under the guidance of senior engineers.
Apply fundamental structural analysis principles to support the assessment and resolution of product and process issues throughout the product lifecycle.
Review of MRB dispositions for structural integrity, helping to identify and document deviations that may affect design intent or safety.
Contribute to developing alternative repair recommendations in collaboration with Liaison Engineering to meet structural requirements.
Assist in coordinating with regulatory agencies and representatives to support certification activities for airplane structural components.
Requirements
Bachelor of Science degree in Engineering (Mechanical, Civil, Aerospace Aeronautical or Material Sciences)
Nice to have: CAD software (Catia)
Nice to have: CAE software (Patran, Hypermesh, Abaqus)
Define, analyze, and validate the loads environments that drive structural design for Project Ranger.
Compensation
Pay within range listed + Bonus + Benefits + Equity
Responsibilities
Develop air vehicle and component level loads analyses for primary and secondary structures.
Create and maintain loads models, free body diagrams, load paths, load cases, design envelopes, and critical load conditions that inform structural sizing, design decisions, and verification planning.
Partner with Aerodynamics, Flight Controls, Mass Properties, Propulsion, and Systems Engineering to define external loads, inertial loads, aerodynamic loads, actuator loads, interface loads, and vehicle operating conditions.
Deliver clear loads documentation, including design load reports, interface control loads, critical condition summaries, assumptions, margins, and recommendations for use by structures, test, and certification stakeholders.
Support ground and flight test planning, instrumentation definition, correlation activities, structural test execution, and post test data analysis to validate models and refine structural loads predictions.
Requirements
Bachelor’s or Master’s degree in Aerospace Engineering, Mechanical Engineering, or a related technical discipline
Nice to have: Master’s degree in Aerospace or Mechanical Engineering with emphasis in structural dynamics, aeroelasticity, aircraft loads, flight mechanics, or a related field
Senior Engineer, Structural Analysis (R6027)
f7d8749a-72d6-407c-bf98-292ea630c73a · Posted Oct 14, 2026
Shield AI is seeking a Sr. Structural Analyst to support the analysis and testing of advanced UAVs, focusing on the structural integrity of lightweight, high-performance aircraft.
Compensation
Pay within range listed + Bonus + Benefits + Equity
Responsibilities
Assist in building and refining finite element models (FEM) to evaluate the structural performance of UAV components.
Perform static, modal, fatigue, and vibration analyses to assess stress, deformation, and durability.
Conduct hand calculations to validate FEA results, ensuring accuracy and structural reliability.
Work with design engineers to optimize airframe structures, balancing weight, strength, and manufacturability.
Support the development of test plans for structural validation, including quasi-static, vibration, and shock testing.
Mid-Level Structural Engineer to join Boeing Commercial Aircraft Structures team and provide support focused on fuselage structural support, non-conformance resolution, and repair development.
Responsibilities
Evaluate the strength and integrity of structural non-conformances and repairs to ensure compliance with safety and design standards.
Apply structural engineering principles to assess and resolve product and process issues throughout the product lifecycle.
Analyze MRB dispositions for structural integrity, identifying, documenting, and communicating deviations that may impact design intent or safety.
Provide alternative repair recommendations for Liaison Engineering to meet structural requirements when necessary.
Support structural design activities, including development and modification of primary and secondary structures as needed.
Requirements
Bachelor of Science degree in Engineering (with a focus on Mechanical, Civil, Aerospace Aeronautical or Material Sciences)
Nice to have: Experience with aerospace structures engineering
Nice to have: Experience with Structures Engineering, including static, fatigue, and damage tolerance analysis
Nice to have: Experience with composite analysis and composite failure modes
Nice to have: Experience with metallic components analysis and metallic joints
Mid-Level Structural Stress Engineer responsible for evaluating and ensuring the structural integrity of aircraft components, primarily fuselage, within Boeing Commercial Aircraft Structures team.
Responsibilities
Evaluate the strength and integrity of structural non-conformances and repairs to ensure compliance with safety and design standards.
Apply structural analysis principles to assess and resolve product and process issues throughout the product lifecycle.
Analyze MRB dispositions for structural integrity, identifying, documenting, and communicating any deviations that may impact design intent or safety.
Provide alternative repair recommendations for Liaison Engineering to meet structural requirements when necessary.
Coordinate with regulatory agencies and representatives to support the certification of structural components.
Requirements
Bachelor of Science degree in Engineering (Mechanical, Civil, Aerospace Aeronautical or Material Sciences)
Nice to have: Experience supporting uncrewed aircraft, fixed wing aircraft, rotorcraft, defense, space, or other aerospace vehicle development programs
Nice to have: Experience developing or correlating loads models using flight test, ground test, structural test, strain gauge, pressure, acceleration, or other instrumentation data
Nice to have: Familiarity with aeroelasticity, flutter, dynamic response, vibration, fatigue, durability, damage tolerance, or nonlinear structural analysis methods