Walk-in || Static and F&DT Engineer

Job Requirements
Technically the job involves investigating and producing F&DT justifications solutions for simple and complex Primary Structural Elements (PSEs) 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.
2-6 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
Static Engineer
Work Experience
Holds relevant technical qualifications (Bachelor, Master or equivalent) or a relevant level of experience to perform the stress engineering tasks.
2-8 years of experience with strong knowledge of airframe static stress including FEA & hand calculation methods.
Sound knowledge of structural design principles, aircraft loads and Airbus manuals.
Experience in Static analysis of aircraft structural components (Airbus methods and tools would be preferable).
Sound knowledge of the overall static structural substantiation process from definition of external loads through airframe finite element analysis to final check stress clearance.
Sound knowledge of Airworthiness Requirements.
Working experience on creating stress justification reports and related stress hand calculations in consultation with Check/Approval signatories.
Have strong working knowledge of. Hypermesh, MSC Nastran, Patran, ISAMI,
Able to execute/check finite element modelling methodology, interpret results and generally design assure the model output.
Strong experience in Metallic - Linear & Non-Linear Static, analysis.
Added advantage with working knowledge of Automation tools like Python and
Supporting continuous improvement initiatives to increase team efficiency.
Support or generate test specifications/plans and/or alternate means of compliance (analysis/similarity) as required to demonstrate design solution complies with certification requirements.