Job Description
At Boeing, we innovate and collaborate to make the world a better place. We’re committed to fostering an environment for every teammate that’s welcoming, respectful and inclusive, with great opportunity for professional growth. Find your future with us.
THE ROLE
BGS EASA Mods are looking for a multi-skilled Senior Stress Engineer to support the certification of large aircraft modifications to demonstrate compliance with relevant regulatory and customer requirements and procedures defined in the company’s Design Organization Handbook (DOH), primarily based out of our Dublin office.
KEY RESPONSIBILITIES
Reporting to the Structures Engineering Manager and working with the global engineering services team, across multiple time-zones, in order to identify requirements and their associated solutions for active and upcoming projects
Lead certification activities to ensure compliance with design requirements, and be a technical focal for certification and stress issues relating to large aircraft modification programmes
Compile and review structural substantiation documents related to:
Product certification and integration to the aircraft of:
New seating installations
New monument and furniture Installations such as Galleys, Lavatories, class dividers, first class suites and VVIP furnishing.
Cabin interior changes including LOPAs, Passenger Service Unit layouts, LRU installations, etc…
Primary structure changes including:
Antenna Installations
Fuselage Modification
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Act as Boeing representative during customer meetings such as ITCM, PDR, CDR and FAI in support of active and up‑coming projects. Provide additional on‑site support to assist the customers’ during the embodiment phase of the project
MINIMUM QUALIFICATIONS
Bachelor’s Degree within Aerospace/Aeronautical Engineering
Equivalent to Eight (8) years relevant experience
PREFFERED SKILLS/EXPERIENCE
Current or recent appointment as an EASA Compliance Verification Engineer (CVE) with terms of approval relevant to the stress/structures discipline (Panel 3) is highly desired
Proficient in hand calculations, using classic stress analysis techniques
Proficient in Finite Element Analysis
Able to demonstrate a comprehensive working knowledge of EASA regulatory and airworthiness requirements including (E)TSO, CS‑25, JAR‑25 and FAR 25 requirements (relevant to the stress/structures discipline)
Knowledge and experience of aircraft interior reconfiguration programmes and primary and secondary aircraft structures
A high level of attention to detail and professional integrity
Ability to work on multiple programmes with varying level of requirements efficiently and effectively
Ability to prioritise workloads and show flexibility to changing situations / demands
ABOUT YOU
A person of integrity who values attributes like trust, honesty and respect.
You enjoy working in a collaborative environment, are willing to share knowledge and wisdom and not afraid to admit limitations.
You are adaptable and resilient with high
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