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Boeing · 1 day ago

Senior Structural Analysis Engineer

USA - Hazelwood, MO

Full-time

Onsite

Senior Level, Lead/Staff

$155K/yr - $209K/yr

9+ years exp

The Boeing Company is seeking a Senior Structural Analysis Engineer to join their F/A-18 Structural Analysis team in Hazelwood, MO. The role involves conducting stress analyses of aircraft primary structures, verifying structural integrity, and providing technical direction to teammates while working with cross-functional teams.

AerospaceIndustrial

No H1B

Security Clearance Required

U.S. Citizen Only

Responsibilities

Conduct stress analyses of aircraft primary structures using well defined analysis tools

Verification of structural integrity by using analytical methods, finite element models/simulations and other analysis tools to develop and maintain the structural environment, characteristics and performance

Supports in-service products by investigating failures and analyzing improvements

Development of test plans and configurations, support test execution and analyses/reports to validate systems and components meet requirements and specifications

Support Configuration Control Board and Engineering Review Board as a Strength Engineering Lead

Provide leadership and technical oversight to other Structural Analysis Engineers

Support on-going supplier and customer activities providing real-time support

Works under minimal direction

Qualification

Structural analysisFinite element modelingAircraft design principlesLeadership in engineeringDocumentationCommunicationTeam collaborationProblem-solving

Required

Bachelor of Science degree in Engineering (with a focus on Mechanical, Civil, Aerospace Aeronautical or Material Sciences)

9+ years' experience in structural analysis (Level 4)

9+ years' experience with building finite element models. Including Fasteners (CELAS, CBUSH, Rutman, etc), Bonded joints, bonded structure that includes honeycomb core, laminate composite details and assemblies, and details FEMs using P-element (Stress Check, Mechanica) solvers

Experience with structural design principles for aircraft primary structure (e.g., fatigue, damage tolerance, corrosion, stress analysis, statics, materials strength, material characteristics, and repair techniques)

Experience analyzing fastened, and bonded joints with metallic and composite details

Experience designing and sizing repairs for primary flight structures

Experience with comprehensive detail documentation and clear communication of complex technical details

Experience in role that required leadership in structural analysis

Experience providing detailed engineering work and schedule estimates for complex projects

Ability and willingness to travel 20% of the time domestically and internationally