Our team had the full responsibility of the Global FE model management (Wing, Center & Aft Fus).

Furthermore, follwing activities were performed:

• Conceptual stress analysis
• Trade studies on wing planform
• Compliance of the wingbox (stiffness, weight, fuel volume)
• Wing CFRP optimization with respect to: loads, stiffness, fuel
• Studies on MLG attachment
• Studies on engine mounts and pylons
• Studies on Center & AFT Fuselage