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Vitor FerrazVF

Durchschnittliche Reaktionszeit: 1h

Über Vitor

I’m a RAMS, Maintenance and CAMO/Part 145 Engineer with over 12 years of experience in Aerospace, Continued/Continuing Airworthiness, inputs to and review of Technical Publications (Maintenance data), and Part 21/CAMO/Part 145. My expertise includes CAMO/Part 145, optimizing system architecture and life-cycle performance, ensuring compliance with airworthiness and industry standards, as well as applying Maintainability principles to reduce downtime and improve system reliability.

Key strengths:

- Led initiatives that reduced system downtime through maintainability and design improvements.
- Contributed to the development of maintainability and maintenance programs for cutting-edge aerospace systems, driving efficiency and reducing life-cycle costs.
- Managed cross-functional teams to deliver aerospace projects on time, on quality, and within budget.
- Provided inputs to and review of Technical Publications in order to support development of approved Instructions for Continued Airworthiness (Maintenance data) for type certification purposes.

I’m excited to contribute my skills in CAMO/Part 145/MRO, Maintenance Planning, Maintainability Engineering, or RAMS to innovative aerospace industry projects. Let’s connect to explore potential opportunities!
  • Englisch

    Verhandlungssicher

  • Spanisch

    Verhandlungssicher

  • Portugiesisch

    Muttersprachlich oder zweisprachig

Nur remote
Führt Projekte hauptsächlich remote aus

Projekt- und Berufserfahrung

  • To be announced later
    RAMS Senior Engineer
    LUFT- & RAUMFAHRT
    Mai 2025 - Heute (1 Jahr und 1 Monat)
    Munich, Germany
    • Developed and maintained Fault Tree Analysis (FTA) and performed Reliability modelling in Isograph based on top event requirement specifications for different flight phases (e.g.: ESA Loss of Mission, ESA SDM/CNES LOS Accidental Spacecraft Break-Up, etc.).
    • Performed and drove qualitative and quantitative FTA as part of Probabilistic Risk Assessments (PRAs), including generation of potential Single Points of Failure reports and participation in joint spacecraft design evaluations with system stakeholders.
    • Coordinated and participated in Technical Interchange Meetings (TIMs) with ESA and NASA regarding RAMS deliverables (e.g., FTA/PRA Plan, Fault Tree Reports, Reliability analyses, and associated documentation) for spacecraft certification purposes.
    • Collaborated with vendors and suppliers regarding Reliability, Availability, and Maintainability (RAM) aspects, including the provision and review of Reliability input data such as Reliability Reports, Failure Rates, Mean Time Between Failures (MTBF), and FMEA results.
    • Ensured, as part of Mission Assurance, that design complied with relevant safety and reliability standards, including NASA, ESA and CNES specifications and requirements.
    • Supported evaluation meetings driven by design review milestones (e.g.: PDR) by assessing and reviewing RAMS deliverables in accordance with the Statement of Work (SOW), ensuring supplier compliance with listed deliverables and requirements, and actively participating in the raising and review of Review Item Discrepancies (RIDs).
    • Cooperated with the Quality Assurance Department in developing Mission Assurance protocols defining RAMS activity workflows - including inputs, outputs, and team interfaces - to support EN9100 certification.
    • Led cross-functional design review sessions with spacecraft system stakeholders to verify compliance with NASA SSP redundancy and fault-tolerance requirements, ensuring robust system reliability and Mission Assurance.
    Fault Tree Analysis (FTA) & Probabilistic Risk Assessment (PRA) RAMS Engineering Mission Assurance & Compliance (ESA, NASA, CNES) Supplier & Stakeholder Coordination Redundancy & Fault-Tolerance Verification
  • Lilium
    Senior Maintainability and Maintenance Engineer
    LUFT- & RAUMFAHRT
    August 2021 - April 2025 (3 Jahre und 8 Monate)
    Munich, Germany
    • Perform detailed Maintainability and Human Factors considerations, accessibility studies and design reviews throughout product life cycle phases (including but not limited to PDR and CDR) alongside multiple IPTs.
    • Enhanced maintenance efficiency by over 30% through comprehensive maintainability and Fault Tree Analysis, optimizing MTTR through reliability data such as MTBF, and ensuring compliance with design standards.
    • Performed Fault Tree and Reliability Block Diagram Analysis with Isograph, evaluating failure severity and integrating PSSAs, SFHAs, and FMEAs to reduce failure risks through a 30% maintenance task optimization.
    • Developed and implemented Fault Tree Analysis-based maintenance concepts by executing maintainability analysis and MTTR allocation, leveraging reliability data (MTBF) to achieve a 15% reduction in maintenance time of certain systems.
    • Drive Design for Maintainability and Design for Maintenance work streams in collaboration with several IPTs.
    • Execute Maintainability analysis, establish Maintenance Concept (including scheduled maintenance based on Fault Tree Analysis), perform Maintainability Allocation for MTTR calculation, based on Safety and Reliability data (including MTBF and other inputs).
    • Serve as EASA Panel 14 DCS while supporting discussions with EASA to ensure compliance with ICA regulatory requirements.
    • Drive development of ICAs in collaboration with relevant stakeholders alongside the Technical Publications team.
    • Responsible for mentoring teammates as the resident expert while translating maintenance data into operative instructions.
    • Provide and enable release to service processes, and secure QA and a suitable control plan with the full value chain.
    • Support and coordinate maintenance planning, scheduled and unscheduled maintenance and modification implementation along with Base Management and Flight-Testing Operations during Flight Test Campaign for Type Certification (TC) purposes.
    Design for Maintainability (DfM) & Maintenance Optimization Maintainability Analysis & MTTR Allocation EASA Certification & ICA Compliance (Panel 14 DCS) Flight Test & Maintenance Operations Support Cross-Functional Integration & Technical Leadership
  • Virgin Atlantic
    Design And Development Engineer
    LUFT- & RAUMFAHRT
    Januar 2018 - Juli 2021 (3 Jahre und 6 Monate)
    London Heathrow Airport, London, England, United Kingdom
    • Experience on Airbus (A330, A340, A350) and Boeing (B747, B787) aircraft.
    • Responsible for engineering technical support under the company's EASA Part-CAMO and Part 145 approvals including: avionics, mechanical systems, cabin, propulsion and programs.
    • Reviewed technical documents and literature issued by aircraft manufacturers, equipment vendors and regulatory bodies.
    • Assessed and recorded implications (TDAs) and recommendation of the appropriate action to ensure continued compliance with regulatory requirements.
    • Liaised with EASA Part 21 Design Organizations for the development or embodiment of modifications or design changes.
    • Provided line/hangar maintenance with MIDA and special check documentation through a combination of information from approved data sources.
    • Served as a technical liaison between the airline, OEMs and regulatory bodies.
    • Responsible for programming, manipulation, analysis and presentation of technical data and recommendations to key stakeholders throughout the business to support technical decision making.
    • Supported the development and review of departmental processes and procedures (EDPs/LOIs).
    • Assessed and supported fleet maintenance and modification policies.
    • Supported project management needs of modification campaigns in collaboration with out-sourced third parties.
    • Assisted in completing safety investigations and closing out ADs and other occurrence reports in accordance with the company's Safety Management System (in conjunction with FTM, Flight Safety and QAG).
    • Conducted defects investigations and implement corrective actions to maintain safety, system integrity, continuous improvement and reliability at optimum cost.
    EASA Part-CAMO & Part 145 Technical Support Airworthiness & Regulatory Compliance Management Modification & Design Change Coordination (Part 21 DOA Interface) Defect Investigation & Reliability Improvement Fleet Maintenance & Data-Driven Decision Support

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Ausbildung und Abschlüsse

  • Aeronautical Engineering
    Universidade da Beira Interior
    2008
    Aeronautical Engineering
  • Industrial Maintenance & Traineeship
    CENFIM
    2013
    Industrial Maintenance & Traineeship

Kategorien

  • Sonstige