Review/perform analyses with hand calculations using OEM and DoD stress methods and industry standards
Initiate complex repairs and prepare static strength/fatigue analysis of engineering repair dispositions for nonconforming aircraft structure
Manage project components including establishing task priorities, scheduling and tracking work assignments, providing guidance, and ensuring the availability of resources
Implement creativity and flexibility in daily activities by relying on experience and judgement to plan and accomplish goals
Use Finite Element Software pre and post processors such as Nastran/Patran and Femap
Develop reports that demonstrate designs and satisfy all relevant design requirements
Provide oversight and technical direction to less experienced engineers
Requirements
7+ years of work experience in airframe analysis
Bachelors or Masters degree in engineering from a U.S. accredited college or university
Mechanical or aerospace engineering preferred
Usable knowledge of aircraft static strength analysis methods, finite element analysis, and strain life fatigue methods
Knowledge of maintenance and repair practices used in the aerospace industry
Experience with designing and substantiating aircraft repairs
Strong communication and interpersonal skills.
Benefits
401(k) plan with immediate 100% vesting and 4% discretionary match
Paid leave including PTO, holiday, bereavement, and military
Generous medical, dental, and vision insurance for employees and their families
Health and dependent care FSA
Company-provided life/AD&D, as well as supplemental life and disability insurance