Structural Design Engineer Job at Airbus (Bangalore)

Job Description

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

Job Responsibility

Vehicle structure Architecture and Design Definition: Define structure architecture and function solutions in accordance with engineering operation 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
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
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.)

Requirements

Bachelor of Science in Mechanical or Aerospace Engineering or similar
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
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
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, Failsalf , 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 ...)
This job requires an awareness of any potential compliance risks and a commitment to act with integrity
Required Competencies: A110: Dev of Sub-syst/Equip/Comp/Mod <CO-E01-00008> (2 - Autonomous Level), A201: Design to requirements <CO-E02-00001> (2 - Autonomous Level), A202: Tolerancing <CO-E02-00002> (2 - Autonomous Level), Collaborative design for Manufacturing <CO-MU_-00021> (2 - Autonomous Level), D027:Certif., Qualif. &/or Airworthiness <CO-D02-00009> (2 - Autonomous Level), D040: Overall Materials & Processes <CO-D04-00001> (2 - Autonomous Level), D050: Overall Mechanics / Structure <CO-D05-00001> (2 - Autonomous Level)

Nice to have

Masters of Science in Mechanical or Aerospace Engineering
Professional Engineer’s License (or eligibility)
Knowledge of structural load / stress analysis

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