Senior Engineer Stress & F&DT

Job Requirements Job Title: Senior F&D Engineer

Job Type: Full-Time

Technically the job involves investigating and producing F&DT justifications solutions for simple and complex Primary Structural Elements (PSE’s) of Wing Structure.

Following are the core responsibilities:

• Work as team offshore member/Team Lead to Support the customer in F&DT stress substantiation for Design deviations in the form of Engineering Analysis using established standards and working procedures • Responsible for delivery of high-quality Static justifications to time, cost and quality requirements • Liaise with the customer SPOC to discuss queries and seek feedback on work delivered. • Ensure Customer and Quest KPI are achieved. • Develop training plan as required and ensure quick job deployment of new Engr added to team.

Work Experience

• Holds relevant technical qualifications (Bachelor, Master or equivalent) or a relevant level of experience to perform the stress engineering tasks. • 3-6 years of experience with strong knowledge of airframe static stress including FEA & hand calculation methods. • Knowledge of static and fatigue design values (Ftu, Fty, Fcy, AFI parameters, S-N curve parameters, fracture toughness etc.,) • Fatigue calculations (Hand calculations, DFEM, ISAMI, GFEM load redistribution) • Calculation of Seq stresses (fatigue and crack propagation), understanding of mission profiles, rainflow counting, Miner's rule, stress files, FESPS databases, Spectra generation. • Calculation of Stress concentration (Kt) values using Petersons' or DFEM or ISAMI modules. • Ability to read the drawings and interpret fastener diameter, fastener fit, fastener spec & type, surface protection treatment to be useful for fatigue calculations. • ISAMI modules (Metallic Filled Hole, Composite Filled Hole, Lug analysis, Corin Analysis, Notch Sensitivity, Damage Tolerance, Tension Fitting, Fatigue Spectrum Analysis (1D & 2D), Fatigue DFEM Initiation Modules, etc.,) • Develop, implement, and check technical solutions and compliance documentation to ensure they are compliant with all relevant customer, regulatory, and airworthiness requirements, within agreed program, schedule, and manufacturing constraints. • Sound knowledge of airframe fatigue substantiation including safe life and fracture mechanics techniques