As a Structural Compliance Certification Engineer, my expertise lies in ensuring that aircraft interior components meet regulatory standards and uphold cabin safety. Previously, I held the position of Senior Stress Engineer in the Design Organization Authority (DOA), where I used advanced analysis methods to check the stress levels of these parts and how they're installed. My main area of expertise lies in understanding and complying with EASA Part 21J regulations. I play a key role in proving that these components are structurally sound and that the aircraft can handle them safely. By focusing on accuracy and following industry standards, I help ensure the safety and reliability of aircraft interiors, prioritizing cabin safety.

In my current role within the Design Organization Authority (DOA), I play a key role in justifying both the stress of aircraft interior parts and the installation of these components. Using finite element and analytical analysis methods, I ensure compliance with EASA Part 21J regulations. This involves not only validating the structural integrity of interior parts but also demonstrating the aircraft's capability to sustain these installations

My primary responsibilities within the Design Organization Authority (DOA) encompass the stress justification of various components, as outlined below. This involves employing finite element (FE) and analytical analysis methods in accordance with EASA Part 21J regulations:Stress justification and installation of composite panel class dividers in the cabin.Justification and installation of the Pilot Tablet assembly support in the cockpit, considering windmilling loads if necessary.Installation of monuments in the cabin, including the justification of cabin provisions and modifications.Installation of emergency equipment in the cabin, coupled with the design and justification of their supports.Equipment installation in the helicopter cabin.Seat cargo bag installation in an aircraft cabin.Planning, witnessing, and reporting on tests for various components

Airbus A350 KB & ALS Test Team LeaderTest leader for the certification of the Airbus A350 Keel Beam & Aft Lower Shell WP. Planning, quality control. Chief of the stress and design activities related to the structural tests.Airbus A330neo AIOS (Air Inlet Outer Surface)Stress analysis, documentation, and quality control required for the certification of the Air Inlet Outer Surface of the A330Neo.Check of the composite FE modelsDevelopment of 2D/3D FE model for an air induct for static and fatigue analysisAirbus A330neo KarmanFE modeling of composite panels.Analysis of customer dedicated composite stress method for Allowable Damage Limits with the implementation of an automated method of analysisStatic and buckling analysis.Damage tolerance analysis

(Le Havre, France): responsible for the finite element modelling and analysis of composite acoustic panels for the nacelle fan duct and thrust reverser of a wide body commercial aircraft.(France, Tolouse): finite element analysis of a satellite battery support.(Cannes La Bocca, France): finite element modelling and analysis of composite sandwich panels for telecommunication satellitesAermacchi: see hereafter

Responsible for the qualification of composite materials, core materials, and adhesives for various commercial aircraft nacelle programs. Support of the stress office and of the manufacturing office in the development and certification of innovative composite structures. Collaboration to the definition of materials and process specifications.

Tactical Control Officer, 1st NATO HAWK Battery, 5th Anti Aircraft Regiment "Pescara"