Airframe Structural Design Engineer Resume

SUMMARY:

9 years of diverse experience in Aerospace Design in the field of Commercial Aircrafts/ Aerospace with specialties in Structural Design Engineering. Extensive experience in designing components, assemblies of fuselage and wing structure, systems integration, interior payloads design. Engineering experience includes design and modification of aircraft structural components/assemblies, design engineering support of fuselage factory assembling process, suppliers support, take part in project for weight and cost reduction. Handling all phases of design including concept & detail design, drafting, signature routing & engineering release from conceptual layouts through production drawings by utilizing CATIA V5/V4, ENOVIA LCA, IVT, PDM, KBE. Working together AND coordination with DE, ME, BMT, DQA as well as other program teams to find optimal design solution. Worked on aircraft structure design projects such as legacy Boeing 777 family planes programs and new modification: 747 - 8F & 747-8I, 777-9.

TECHNICAL SKILLS:

Computer skills: CATIA V5 (Part Design, Assembly Design, Generative Shape Design, Surfacing, Sheet Metal, MBD, Sketcher, 3D models, 2D Drafting, etc.)& ENOVIA LCA, PDM; CATIA V4; KBE, Relational Design (ICMs/RLMs based design),v4-v5 Conversion; GD&T, ASME Y14.5-2009, MS Windows; MS Office; variety of Boeing tools (REDARS, DIOL, Bridge, IVT etc.).

Personal skills: Result oriented. Process approach. Accurate. Responsible. Follow through to investigate and resolve problem issues. Produce high quality work.

WORK EXPERIENCE:

Airframe Structural Design Engineer

Confidential

Responsibilities:

777 - 9 DOORS Create new drawing and new design - creating new drawing of details, assembles and modules for doors and new design of detail parts and assemblies, update 3D models of details and assembles, update modules drawing, work with packages for the release process.
747-8I Section 44 Modification - creating new design of detail parts (frames, intercostals, stringers) and assemblies, creating drawing of details, assembles and modules for door 3 CATIA v4-v5 conversion 747 Section 44 - conversion V4 models to V5 models of details, assembles and installations, conversion V4 drawing to V5 drawing of details, assembles and installations.
747-8F and 747-8I Fuselage Airframe Sections 42, 44, 46, 49 Sustaining - Factory DE Support;
Investigating of engineering issues and discrepancies related to aircraft structure design that arise during the production of the Aircraft by working factory CARs and Boeing/Supplier s ECR/ELRs; clarify questions that arise during investigation by communication with airframe leadership (Mechanics, ME, BR&T, Stress);
Creating/revising 3D/2D CATIA V5 datasets, CARMs and PDM, ENOVIA PLs of various primary body structure details such as shear-ties, stringer clips, stringers, ribs, stiffeners, fittings, frames, skins, etc., Section 44 Skin Panels, Bulkheads STA 1480/1350, Doors, Landing Gear assemblies and modules to improve structure design, fix various issues and provide Boeing/Suppliers with valid documentation to deliver actual plane configuration;
Interacting closely with other program teams such as Systems, Payloads, Tooling to integrate Section 44, 46 data requirements;
Coordinating technical tasks and develop, change and modify CATIA v5 datasets, CARMs, IRMs, ERMs. release packages by sent to Everett team for signature routing;
Supporting and coordinating the workflow between Everett, Moscow and suppliers teams;

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