Management of type certification processes.Approval of changes to type certificate and repair projects.Management of type validation processes for Vulcanair products all over the world.Approval of Flight Conditions for experimental flights.

CVE (Structures and Cabin Safety, Hydromechanical Systems).Approval by signing compliance documents concerning the relevant technical area (only minor change).Aircraft: Vulcanair V1, P.68 and AP68TP series

Approval of minor changes and minor repairs, minor revisions to aircraft flight manuals, new issues or revisions of equipment lists, service documents (i.e. AMM, IPC, SB, SI, SL) and of OSD.Involvement in the certification project of major changes and management of minor changes in accordance with Part 21 (para. 21.A.91, 21.A.95, 21.A.97, 21.A.101) and associated compliance documents. Complete occurrence treatment, resolution and closure with preparation of related final report.

Preparation and management of the complete set of technical publications (Flight Manual, Maintenance Manual, Illustrated Parts Catalogue, Service Bulletins, Service Instructions, Service Letters, Repair Schemes, Equipment List) concerning the Vulcanair fleet.Management and collection of all data and technical reporting coming from the customers and/or Vulcanair departments concerning the Occurrences that may involve failures, malfunctioning and/or defects, in accordance with Part 21 (para. 21.A.3A), coordination of all necessary actions in order to provide suitable replies and guarantee the Continued Airworthiness of the Vulcanair fleet.Involvement in the Continued Airworthiness review meeting and preparation of related Minute of Meetings. Involvement in the validation process of Vulcanair fleet and in the subsequent validation visit in Italy and abroad (China – Shenyang), support to the involved foreign Civil Aviation Authority, preparation of technical documents for the certification activities.

Fatigue and DT calculations in the pre-design & design phases of the A319/A320/A321 NEO project. Realization of Fatigue job cards for the program A320 NEO with F&DT Justification (ACD6) and Fatigue Maintenance tasks (MRB, ALI) for maintenance impact on airlines operating on A320 aircraft.Starting from Parametric study and pilot points classification on A320 nose-fwd fuselage section (S11/12/13/14) and CWB (S21), extraction of static and fatigue internal loads (GFEM), Global Mapping plus critical points and definition of range effect on fatigue spectrum and propagation.Fatigue Life and Intervals F&DT status, in order to present potential zones for reinforcements or re-design. Static and Fatigue strength analysis for system cabin installation (SEI) in frequency range windmilling. Static, Fatigue and DT certification activities.Realization of fatigue certification dossiers for the program A350 XWB MLGB.Starting from global finite element (GFEM), extraction of static and fatigue internal loads.Use of 3D modelling (DFEM).Fatigue analysis of holes, pockets and junctions (DT and Crack Propagation on Stabilizer, Horizontal Panel, Vertical Panel and Frames) with Airbus methodology, IQF - AFI definition and SAFE analysis.

Fatigue analysis of hybrid junction (DT and Crack Propagation on Gantry and Bulkhead) with Airbus methodology, IQF definition and SAFE analysis.Activity of analysis and documents for aircraft certification program A380.Static and fatigue analysis (DT and Crack propagation) for typical zone (Fuselage – stiffened panel) and for no typical zones (Door surrounds, window frame, joints).Preparation of preliminary/definitive interface loads and preliminary/definitive stress notes for several Interiors parts to aircraft customization. Definition of finite element model, loads and boundary conditions, post processing to analyze interface junctions and structures (composite and metallic materials). Re-analysis and Margins assessment, considering the latest update of Loads, Methods and Allowable. Check of the APARD parameters used as input in the Boeing Analysis Tools (FAMOSS, IAS templates) before running any margin assessment.Preparation and control for the static, fatigue and damage tolerance stress dossiers (SCN).

Research and DevelopmentActivity test for qualification of the Structural Monitoring Process of composite parts through Fiber Optic Sensors (FOBG).Preparation and control for the static, fatigue and damage tolerance stress dossiers.

Research and DevelopmentStructural Health Monitoring through the development of Fiber Optic Sensors (Bragg Gratings), the traditional Strain Gauges and the acoustic emission techniques.