F&DT Engineer

Job description

**Work Experience** - Holds relevant technical qualifications (Bachelor, Master or equivalent) or a relevant level of experience to perform the stress engineering tasks. - 3-10 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