Job Description SummaryIn this role person demonstrates technical expertise in leading projects to achieve program goals within the program schedule and processes. In this role you will lead in a cross functional team working on GE Aviation commercial engines like GEnx, GE9X, GE90 and GP. You will be responsible for engine critical parts to certify safe and competitive life limits for entire product life cycle.Job Description
In this role, you will report to Life Management Sub- Section Manager, BEC, JFWTC Bangalore. You will be responsible for engine critical parts to certify safe and competitive life limits for entire product life cycle. Additionally, you need to proactively resolve field issues, enable repairs and serviceable limits. You will interface with other teams such as Life Cycle Engineering, Services Engineering, Systems, Projects, collaboration with FAA, EASA and agencies based on business need.
In-depth understanding on solid mechanics
In-depth understanding of mechanical/thermal engineering fundamentals
Sound knowledge on Fatigue (LCF and HCF) and Fracture mechanics
Good Understanding on manufacturing process and rotor hardware
Experience in mechanical component analysis (FEA/CAE) and design
Own and execute critical parts life management programs, repairs and serviceable limits using sound engineering principles and adhering to business standards, practices, procedures, and product / program requirements
Collaborate and Communicate with all stakeholders on project status, business issues and significant developments as appropriate.
Collaborate with regulatory agencies like FAA, EASA and deliver life reports/technical memorandums for assigned programs.
Contribute to Life Management Digital play book.
Assure proper documentation of technical data generated for the assigned projects and/or tasks consistent with engineering policies and procedures.
Demonstrate clear thinking, strong technical articulation, manage hand-offs between different organizations.
Foster and inspire a collaborative work style and display team-oriented behavior with a proactive example of communication internally and externally.
Qualifications/Requirements
PhD / MTech / MS / BE from an accredited university or college in Mechanical, Aerospace, Structural Engineering.
4+ years of experience in Aviation Engines or Turbo machinery Engineering position (design, analysis, systems, services)
In-depth understanding on solid mechanics
In-depth understanding of mechanical/thermal engineering fundamentals
Sound knowledge on Fatigue (LCF and HCF) and Fracture mechanics
Good Understanding on manufacturing process and rotor hardware
Experience in mechanical component analysis (FEA/CAE) and design
Strong project management skills including cross-functional coordination of activities
Strong Design creativity and problem solving capabilities
Ability to communicate effectively with all levels of the organization both internally and externally
Desired Characteristics
Good Knowledge on Field failures and manufacturing processes
Experience with engine field problem resolution
Familiarity with aircraft flight operations, engine performance, thermal and stress analysis
Exposure to FAA requirements for life limited parts
Strong oral and written communication skills
Additional Information
Relocation Assistance Provided: Yes
