Aeronautical Engineering for Development & Certification of BVLOS UAS.- Preparation of technical documentation to demonstrate compliance with applicable ANAC requirements, covering RPAS detailed systems description, definition of the Concept of Operations (ConOps), operation risk assessment based on the SORA methodology, Functional Hazard Analysis (FHA), Operation Manual and Maintenance Manual.- Proposal and execution of flight tests to evaluate the behaviour, performance and response of the UAS to simulated failure conditions, followed by the preparation of test results reports.- Close collaboration with global UAS manufacturers and Brazilian aviation authorities, namely ANAC and DECEA, to validate means of compliance and to obtain Airspace flight authorization- Planning and coordination of simultaneous projects, establishing milestones and deadlines.

● May 2021 to August 2021: Structures Engineer - C-390 Millenium Full Scale Fatigue Test- Structures engineer for the C-390 aircraft full scale fatigue testing, analyzing the findings, and providing repair solutions for the test unit.● December 2020 to April 2021: Structures Engineer - C-390 Millenium Allowable Damage Analysis- Conducted the allowable damage analysis and prepared certification reports for the C-390's rear fuselage, pod pylon, and horizontal stabilizer structures.

- Engaged as a stress analysis engineer for the Gripen E and Gripen F aircraft in the cooperation program between Embraer and SAAB.- Performed hand and finite element analysis of the Gripen E/F fuselage, with static and fatigue analysis of frames, spars, and skins.

● January 2017 to March 2018: Praetor 600 Executive Jet - Stress Analysis Engineer and team focal point:- Conducted static stress analysis on various sections of the fuselage, vertical tail, wing-to-fuselage fairing, and auxiliary fuel tanks of the Praetor 600 Executive Jet.- Oversaw a team of seven engineers, responsible for planning and coordinating team deliverables to meet project deadlines.● December 2013 to December 2016: Embraer 190E2 and 195E2 Stress Analysis Engineer- Static stress analysis on metallic structures, including spars, stringers, skins, and ribs of the wingtip on Embraer 190E2 and 195E2 aircraft.- Static stress analysis on composite structures, specifically fairings of the 190E2 and 195E2 wingtip.- Fatigue and damage tolerance analysis of the critical parts in the 190E2 and 195E2 wingtip and wing leading edge. Evaluation of fatigue life, threshold and intervals of inspection using in-house tools for fatigue analysis and Nasgro software for crack propagation analysis.- Proficient in finite element modeling and post-porcessing using CAE software such as Hypermesh and FEMAP.

Technical Support on aircraft maintenance activities, developing and submitting to Airbus modifications and repair proposals for damages not covered by the aircraft Structure Repair Manual (SRM), working mainly with the Airbus A320 family aircrafts and the A330.

Intern at LATAM MRO, structures technical support