Principal Stress Engineer

Airbus•Wichita, KS

3d•Onsite

About The Position

Airbus Commercial Aircraft is looking for a Principal Stress Engineer to join our Engineering department based in Wichita, Kansas or Mobile, Alabama. This position supports the production concessions of aircraft structure and is responsible for quality justifications from a static stress point of view in a timely manner. Duties include performing stress analysis for both metallic and non-metallic parts while working in close collaboration with design colleagues to provide solutions. Methods include the use of both classical hand calculations and computer techniques to develop efficient solutions to satisfy airworthiness requirements. The role involves ensuring the safety, efficiency, and regulatory compliance while adhering to the terms of the concession.

Requirements

Bachelor of Science (BS) Degree in Engineering (Aero, Civil, Mechanical).
Minimum thirteen (13) years total experience in stress analysis with airframe structures.
Position requires in-depth knowledge of classical and numerical (Finite Element) stress analysis methods.
Capable of working in a dynamic, fast-paced environment both independently and collectively.
Dependable, self-motivated and accessible.
Team player demonstrating a positive & collaborative attitude.
Able to lead teams technically to achieve agreed milestones.
Demonstrates a refined approach to communication that resolves problems, facilitates consensus, and focuses on objectives
Able to represent Engineering in presentations at any Airbus related activity
Strong computer background, including MS Excel and Google Suite application experience (Docs, Sheets, Slides, Gmail)
Must be able to communicate effectively in English (verbal and written).
Authorized to Work in the US.

Nice To Haves

Experience in airframe design (metallic & composites), stress analysis, SRM, MRB, FAR/JAR/CS/Part21, Certification, CATIA, NASTRAN, and PATRAN, is desired.

Responsibilities

Autonomously perform unusually complex stress calculations for metallic, composite and hybrid structures to assess design solutions for manufacturing non-conformities, airframe repairs and reworks, and modifications to the aircraft definition.
Ensure appropriate Airbus methods, processes and procedures are followed.
Liaise with and support stakeholders such as Design, Manufacturing, Quality and other Airbus departments as necessary to come up with optimum solutions and ensure Stress requirements are fully integrated.
Develop and maintain component / aircraft familiarity, to ensure prompt response to build.
Develop towards and maintain Technical Signature Delegation for concessions for primary and secondary aircraft structures (T400) across multiple suffixes.
Check and Approve / Pre-approve stress justification for non-conformity or modification.
Develop and mentor other Engineers in all types of metallic and/or non-metallic structural repairs.
Drive and execute localized continuous improvement projects, optimizing operational efficiency by advancing internal processes, methodology, and technical tooling.

Benefits

Competitive base salary
Incentive compensation which may include profit sharing schemes
Retirement savings plan
Employee Stock Ownership Plan (“ESOP”)
Paid time off including personal time
Holidays
Generous paid parental leave program
Comprehensive insurance coverage including medical (traditional and high-deductible health plans), prescription, dental, vision, life, disability, Employee Assistance Plan (“EAP”) and other supplemental benefit coverages.
Upskilling and development opportunities through our global Leadership University
Unlimited access to 10,000+ e-learning courses
Accelerated development programmes
National and international mobility