Structural Design Engineer – Design at airbus

Job Description:

Latest job information from airbus for the position of Structural Design Engineer – Design. If the Structural Design Engineer – Design vacancy in Bengaluru matches your qualifications, please submit your latest application or CV directly through the updated Jobkos job portal.

Please note that applying for a job may not always be easy, as new candidates must meet certain qualifications and requirements set by the company. We hope the career opportunity at airbus for the position of Structural Design Engineer – Design below matches your qualifications.

Job Description:

Description of the Job:

Airframe team at Airbus India is looking for a Design Engineer to join the Structural Design team in Airbus India, Bangalore.

Job scope (Tasks & accountabilities):

Vehicle structure Architecture and Design Definition 
Define structure architecture and function solutions in accordance with engineering operation requirements as elaborated during offer phases to meet customer, airworthiness, general engineering standards and company requirements.
Design, integrate and approve the defined solutions & Design data sets.
Define and review technical documents needed to verify the structure architecture and relevant product structure.
Define and approve verification methods (analysis, tests…), elaborate verification programs including general engineering aspects such as Function Hazardous Analysis, EMI:EMC, general environment, vibrations, thermal analysis (list not limited) and deliver the verification results to the Airworthiness team.
Provide technical design analysis of third-party STCs
Assess CR change impact on legacy product & implement valid design solution to close MOD/MP’s.

Structural Integration Activities 
Design, develop, and review technical documents and engineering structural drawings needed to integrate equipment and their associated interfaces.
Design layout of aircraft modifications and aircraft configuration for various Programs.
Drafting and 3D modeling of installations, assemblies and parts including sheet metal, metallic  and composite design
Check Wiring Diagrams, wire routing and aircraft structure interface (including considerations of ESI/MSI requirements, separation requirements, maintainability, etc.)
Check airframe design integrations and modifications for structural items such as doors, windows, frames, etc. and for external load items such as cameras, lighting, hoists, cargo hooks, floats, etc.
Review Installation Instructions and Instructions for Continued Airworthiness
Provide liaison support to various internal and external customers as required for support of aircraft integration and conformity efforts (suppliers, planning, industry, quality, etc.)

EDUCATION & JOB REQUIREMENTS 
Education:
Bachelor of Science in Mechanical or Aerospace Engineering or similar
Masters of Science in Mechanical or Aerospace Engineering considered an asset
Professional Engineer’s License (or eligibility) considered an asset
Experience:
6 years’ of dedicated experience in vehicle architecture or structural design of commercial aircraft.
2 years’ Experience in project engineering and project coordination
Experience interfacing with a manufacturing environment/requirement.
Specialist in Catia V5 & Airbus PDM/PLM. (Proficiency Level-2 and above)
Specialists in product component design, assembly, installation & HnF selection. 

Knowledge, Skills, Demonstrated Capabilities:
Accurate, clear, and timely completion of tasks necessary to develop aeronautical products.
Strong initiative and motivation necessary to work independently and in a team environment to drive development.
Ability to learn, understand, and follow department and company procedures
Ability to bring the context of long term strategic objectives and goals and apply them to day to day activities and decisions making (keep the big picture in mind).
Knowledge of vehicle architecture and system integration
Knowledge of  Electrical Wiring Diagram
Knowledge of Tolerancing, HnF, Design principles, RSDP & Aircraft Modeling Rules.
Knowledge of structural aeronautical design constraints
Knowledge of aeronautical materials (metallic, composite …), on their characteristics, mechanical properties, manufacturing process, and pro/cons for their use in design
Knowledge of Aircraft performance and loads applied on aircraft in general
Knowledge of verification methods for general engineering aspects (D2C, Failsafe , vibrations, lightning strike, bird impact, thermal analysis …)
Knowledge of Commercial Aircraft fuselage (doors, canopy, cowling …) and airframe design, and inboard and outboard systems (hoist, seats, console ...).
Knowledge of structural load / stress analysis is considered an asset

This job requires an awareness of any potential compliance risks and a commitment to act with integrity, as the foundation for the Company’s success, reputation and sustainable growth.

Required Competencies:
A110: Dev of Sub-syst/Equip/Comp/Mod (2 - Autonomous Level), A201: Design to requirements (2 - Autonomous Level), A202: Tolerancing (2 - Autonomous Level), Collaborative design for Manufacturing (2 - Autonomous Level), D027:Certif., Qualif. &/or Airworthiness (2 - Autonomous Level), D040: Overall Materials & Processes (2 - Autonomous Level), D050: Overall Mechanics / Structure (2 - Autonomous Level)
 

This job requires an awareness of any potential compliance risks and a commitment to act with integrity, as the foundation for the Company’s success, reputation and sustainable growth.

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