- Manage and integrate the FEM models of all partners into the Global FEM- Interface with Loads Group for the preparation, release and refinement of Load Loops with weight saving considerations- Define the Wheels up landing scenario and participate in the optimization of the concerned structure to reduce the impact loads- Develop a Complete Aircraft Static Test (CAST) FEM model including all loading pads locations to define the actuators loads matching the Shear, Bending, Torque envelope and correlate the CAST strain level with the Global FEM - Model/analyze and optimize the non-linear Integrated FEM model of the Engine-Fuselage interface

Cseries Stubwing/Pylon Implementation on PW747- Model/analyze and optimize the Aft fairing assembly- Perform different static analysis and optimization of the wing box structure: holed panel buckling employing material nonlinearity (Ansys), crippling, column buckling, fastener dimensioning.

Hoist Kit Implementation on model 429- Define static and fatigue load cases leading to certification.- Superimpose the hoist and flight loads to analyze the effect on 429 structure. - Participate to the PDR & CDR with the hoist manufacturer BF Goodrich- Elaborate different solutions, model and analyze the hoist on Patran/Nastran, its attachments and the structural section needing reinforcement (Mid lift frame, Aft lift frame, back up fitting, strap, splice, brace, ...).- Analyze the basic A/C weight impact of different fatigue spectrum to define the weight penalty of certifying a higher maximum human external cargo load.- Perform static and fatigue analysis and optimization for the Mid Lift Frame, back-up structure and attachments based on the chosen spectrum. - Verify fail-safe scenarios at ultimate load.- Prepare certification reports.Certification report on model 429Analyze and prepare the certification report for primary structure: Roof Beam, Lift frames, Lift Frame splices.

- Model by finite element the structure of different cabinets (bulkhead, galley, seat) and analyze the reaction and deformation in the composite panels using generative structural analysis (GSA) from Catia V5. - Propose attachment modifications to obtain positive margin of safety for certification. - Prepare certification reports for cabinets submitted to crash accelerations.- Participate at the process continuous improvement by developing better practices and new strategies for the client.