SC-VTOL EASA Certification Course
About our
EASA SC-VTOL Certification Course
This course provides essential knowledge of the European Union Aviation Safety Agency (EASA) regulations applicable to vertical takeoff and landing (VTOL) aircraft, specifically in the “Special Condition” (SC) category. It covers the safety engineering, design, manufacturing, and operation of these innovative aircraft. It focuses on meeting certification and homologation requirements to ensure the safety and efficiency of VTOL systems, including risk analysis, flight simulation, and compliance with CS-27 and CS-29 standards, as well as new VTOL-specific requirements.
The course prepares professionals for roles such as certification engineers, aircraft designers, and VTOL operators, equipping them to apply the latest safety analysis techniques and understand operational safety management in the context of urban air mobility. The importance of accident investigation and continuous safety improvement in the VTOL industry is emphasized, preparing to face market challenges.
SC-VTOL EASA Certification Course
- Format: Hybrid
- Duration: 3 months
- Hours: 300 H
- Language: English / Spanish
- Registration date: 23-10-2026
- Start date: 12-12-2026
- Available places: 3
620 $
Competencies and results
What you will learn
1. In-depth knowledge of SC-VTOL: EASA certification and its key components
- SC-VTOL Fundamentals: Understand the definition, classification, and applications of SC-VTOL. Explore the evolution of the technology and current market trends.
- EASA Certification and Aeronautical Regulations: Become familiar with the EASA certification requirements for SC-VTOL aircraft. Analyze applicable regulations, including CS-23, CS-27, and CS-VTOL.
- SC-VTOL Architecture and Design: Study the different types of SC-VTOL configurations (tail, tiltrotor, etc.). Analyze aerodynamic design principles, including lift, drag, and stability.
- Propulsion and Control Systems: Investigate electric, hybrid, and conventional propulsion systems. Understand flight control systems, including software and hardware.
Advanced Structural Analysis:
Analyze flap-lag-torsion couplings, whirl flutter, and fatigue.
Dimension laminates in composites, joints, and bonded joints with FE.
Implement damage tolerance and NDT (UT/RT/thermography).
Aerodynamics in SC-VTOL: Examine CFD modeling for rotor and wing flow simulation. Analyze rotor design, including airfoils and performance analysis.
Electronics and Avionics Systems: Study electrical systems, including batteries, inverters, and motors. Understand navigation, communication, and flight control systems.
Simulation and Flight Testing: Learn to use simulation software for SC-VTOL design and analysis. Become familiar with flight testing and certification procedures.
Safety and Operational Aspects: Analyze safety and risk factors in SC-VTOL operation. Study air traffic regulations and safety procedures.
The Future of SC-VTOL: Explore emerging trends in SC-VTOL technology, including artificial intelligence, autonomy, and urban air mobility.
2. Detailed Analysis and Optimization of the Performance of SC-VTOL Rotors with EASA Certification
- In-depth analysis of critical aeromechanical couplings, including flap-lag-torsion, to understand their impact on rotor stability and dynamic behavior.
- Evaluate and mitigate the risks associated with whirl flutter, a potentially destructive vibratory phenomenon, through advanced analysis and design techniques.
- Understand the fatigue mechanisms in SC-VTOL rotors and apply methodologies to predict service life and ensure structural safety.
- Master the laminate dimensioning process in composites, including material selection, layer definition, and design optimization to maximize strength and minimize weight.
- Design and analyze joints and bonded joints using finite element (FE) techniques to ensure structural integrity and Efficient load transfer.
Apply the principles of damage tolerance, evaluating the structure’s capacity to withstand damage and prevent catastrophic failures.
Implement non-destructive testing (NDT) methods, such as ultrasonic testing (UT), radiography (RT), and thermography, to detect defects and assess component integrity.
3. Comprehensive user-oriented design and validation (from modeling to manufacturing)
You will learn to integrate the entire product development process, from initial model conception to final validation, applying user-centered methodologies. You will develop skills in parametric design, ergonomics, simulation, sustainable materials, 3D visualization, and manufacturing management, ensuring efficient, safe solutions that meet current industry standards.
4. Expert Domain: Modeling and Performance of SC-VTOL Rotors with EASA Certification
4. Expert Domain: Modeling and Performance of SC-VTOL Rotors with EASA Certification
- Comprehensive evaluation of SC-VTOL rotor dynamics, including the analysis of flap-lag-torsion couplings, crucial for stability and control.
- Advanced study of aeroelastic phenomena such as whirl flutter, a determining factor in operational safety, and the evaluation of material fatigue.
- Detailed structural design, encompassing the dimensioning of laminates in composites, optimizing strength and weight.
- Finite Element (FE) analysis of joints and bonded joints, ensuring structural integrity under various loads.
- Application of damage tolerance methodologies, including the analysis of crack propagation and behavior under stress.
failures.
Proficiency in Non-Destructive Testing (NDT) techniques, such as Ultrasonic Testing (UT), Radiography (RT), and Thermography, for component inspection.
5. Advanced Evaluation: Modeling and Performance of SC-VTOL Rotors for EASA Certification
- Understand the complex flight dynamics of SC-VTOL rotors, including detailed analysis of flap-lag-torsion couplings, essential for stability and control.
- Evaluate the susceptibility to whirl flutter, a critical phenomenon that can lead to catastrophic structural failures, and learn how to mitigate it through design and analysis techniques.
- Delve into the fatigue mechanisms of SC-VTOL rotors and develop strategies to extend their service life, considering cyclic loading and environmental conditions.
- Master the dimensioning of composite structures, from material selection to the configuration of optimized laminates to withstand the specific loads of the rotors.
- Apply FEA (Factory Element Analysis) methods.
Finite methods for the design and analysis of joints and bonded joints, ensuring structural integrity and efficient load transfer.
Implement damage tolerance principles, evaluating the impact of defects and damage on the rotor structure and defining inspection and maintenance criteria.
Learn and apply NDT (Non-Destructive Testing) techniques, including UT (Ultrasound), RT (Radiography), and thermography, to detect and evaluate internal defects without damaging the structure.
6. Advanced Modeling and Performance Evaluation of SC-VTOL Rotors for EASA Certification
6. **Advanced Modeling and Performance Evaluation of SC-VTOL Rotors for EASA Certification: What Will You Learn?**
Apply advanced methodologies to ensure safety and durability: implement damage tolerance, which assesses the structure’s ability to withstand damage; and master non-destructive testing (NDT) techniques such as UT (ultrasound), RT (radiography), and thermography, essential for the early detection of defects and compliance with certification requirements.
Who this program is for:
SC-VTOL EASA Certification Course
- Graduates in Aerospace Engineering, Mechanical Engineering, Industrial Engineering, Automation Engineering, or related fields.
- Professionals from OEM rotorcraft/eVTOL, MRO, consulting, technology centers.
- Flight Testing, certification, avionics, control, and dynamics seeking specialization.
- Regulators/authorities and UAM/eVTOL professionals requiring compliance skills.
Recommended qualifications: foundation in aerodynamics, control, and structures; ES/EN B2+/C1. We offer bridging tracks if you need them.
- Standards-driven curriculum: you will work with CS-27/CS-29, DO-160, DO-178C/DO-254, ARP4754A/ARP4761, ADS-33E-PRF from the first module.
- Accreditable laboratories (EN ISO/IEC 17025) with rotor bench, EMC/Lightning pre-compliance, HIL/SIL, vibrations/acoustics.
- Evidence-oriented TFM: safety case, test plan, compliance dossierand operational limits.
- Mentored by industry: teachers with experience in rotorcraft, tiltrotor, eVTOL/UAM and flight test.
- Flexible modality (hybrid/online), international cohorts and support from SEIUM Career Services.
- Ethics and security: safety-by-design approach, cyber-OT, DIH and compliance as pillars.
Module 2 — Detailed Analysis and Performance Optimization of SC-VTOL Rotors for EASA Certification
2.1 Rotor Aerodynamics: Blade Element Theory (BEM) and CFD
2.2 Aerodynamic Design: Airfoil Selection and Twist
2.3 Performance Analysis: Power, Thrust, and Efficiency
2.4 Design Optimization: Iterative Techniques and Algorithms
2.5 Wake Effects: Modeling and Mitigation
2.6 Noise and Vibration: Analysis and Strategies
2.7 Structural Design: Materials and Stress Analysis
2.8 Control Systems: Concepts and Strategies
2.9 Experimental Validation: Wind Tunnel and Flight Testing
2.10 Rotor Integration: Aircraft Compatibility
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Module 3 — Comprehensive Analysis: Modeling and Optimal Performance of SC-VTOL Rotors for EASA Certification
3.1 Computational Modeling: Advanced CFD and BEM
3.2 Rotor-Fuselage Interaction: Modeling and Simulation
3.3 Effects Leading Edge Design: Simulation and Analysis
3.4 Design for Specific Flight Conditions
3.5 Stability and Control Analysis
3.6 Multi-Objective Optimization: Design and Performance
3.7 Noise Reduction: Strategies and Simulations
3.8 Validation and Verification: Methods and Tools
3.9 Certification Considerations: EASA Requirements
3.10 Case Studies: Analysis of Existing Designs
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Module 4 — Expert Domain: Modeling and Performance of EASA-Certified SC-VTOL Rotors
4.1 High-Fidelity Modeling: Advanced Methods
4.2 Computational Fluid Dynamics (CFD) in Detail
4.3 Acoustic Noise Modeling: Methods and Analysis
4.4 Transient Rotational Aerodynamics
4.5 Parametric Design and Optimization of Rotors
4.6 Flight Control Systems: Simulation and Design
4.7 Integrating Rotors into Aircraft Design
4.8 Sensitivity and Robustness Analysis
4.9 Meeting Certification Requirements EASA
4.10 Rotor Project Development: From Design to Certification
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Module 5 — Advanced Evaluation: Modeling and Performance of SC-VTOL Rotors for EASA Certification
5.1 Advanced Modeling of Rotor Aerodynamics: High-Fidelity Methods
5.2 Modeling and Simulation of Rotor-Rotor Interaction
5.3 Analysis and Optimization of Rotors for Flight Under Different Conditions
5.4 Simulation of Flight Dynamics and Control
5.5 Advanced Optimization Techniques Applied to Rotor Design
5.6 Analysis of Rotor Behavior Under Failure Conditions
5.7 Risk Analysis and Mitigation in Rotor Design
5.8 Validation and Verification Methodologies for EASA Certification
5.9 Detailed Review of EASA Certification Requirements for Rotors
5.10 Case Studies: Examples of Certified Rotor Designs
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Module 6 — Advanced Modeling and Performance Evaluation of SC-VTOL Rotors for Certification EASA
6.1 Advanced Aerodynamic Modeling: CFD and Moving Mesh Methods
6.2 Rotor-Wake Interaction Simulation
6.3 Stability and Control Analysis in Flight
6.4 Multidisciplinary Rotor Design Optimization
6.5 Noise and Vibration Reduction Techniques
6.6 Rotor Design for Extreme Conditions
6.7 Rotor Failure and Reliability Analysis
6.8 EASA Certification Process for Rotors: Specific Requirements
6.9 Experimental Validation and Wind Tunnel Testing
6.10 Case Studies: Rotor Designs and Their Certifications
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Module 7 — Specialized Modeling and Performance of SC-VTOL Rotors: Key to EASA Certification
7.1 Specialized Aerodynamic Modeling: High-Accuracy Methods
7.2 Simulation of Transient Flow Effects and Separation
7.3 Rotor-Flowwork Interaction Analysis with Advanced Methods
7.4 Rotor Optimization for Different Missions
7.5 Design of Active Control Systems Vibrations
7.6 Modeling and Simulation of Aeroelastic Phenomena
7.7 Rotor System Safety and Reliability Analysis
7.8 Detailed Compliance with EASA Certification Requirements
7.9 Advanced Testing and Experimental Validation of Rotors
7.10 Case Studies of EASA Certifications of Complex Rotors
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Module 8 — Optimization of SC-VTOL Rotor Modeling and Performance: EASA Certification Requirement
8.1 Advanced Aerodynamic Modeling and CFD Techniques
8.2 Rotor Design Optimization to Minimize Noise
8.3 Strategies to Improve Rotor Energy Efficiency
8.4 Modeling Rotor Dynamics under Complex Flight Conditions
8.5 Stability and Control Analysis in Critical Scenarios
8.6 Vibration Mitigation Techniques and Modal Analysis
8.7 Design and Analysis of Advanced Flight Control Systems
8.8 EASA Certification Process: Documentation and Compliance
8.9 Testing and Validation of Prototypes Rotors
8.10 Application of acquired knowledge in real projects
2.2 SC-VTOL Fundamentals: Components and EASA Certification
2.2 Rotor Structure and Design: Key Principles
2.3 SC-VTOL Rotor Aerodynamics: Detailed Analysis
2.4 Optimization Methods: Design and Performance
2.5 Simulation Tools: Practical Applications
2.6 Data Analysis and Performance Evaluation
2.7 Design for EASA Certification: Specific Requirements
2.8 Rotor Integration: Systems and Components
2.9 Case Studies: Applications and Challenges
2.20 Performance Evaluation: Metrics and Results
3.3 Fundamentals of SC-VTOL Rotor Aerodynamics
3.2 Conceptual Design and Rotor Selection
3.3 Flight Dynamics and Stability Modeling
3.4 Rotor Performance Simulation under Various Conditions
3.5 Sensitivity Analysis and Design Optimization
3.6 Noise and Vibration Considerations
3.7 Rotor Integration with the Flight Control System
3.8 Specific EASA Certification Requirements for Rotors
3.9 Rotor Model Testing and Validation
3.30 Case Studies and Industry Examples
4.4 Introduction to SC-VTOL Rotor Aerodynamics
4.2 Computational Modeling of Rotors: CFD and BEM
4.3 Rotor Blade Design: Geometry and Airfoils
4.4 Performance Analysis: Lift, Drag, and Efficiency
4.5 Computational Fluid Dynamics (CFD) Applied to Rotors
4.6 Structure and Materials: Design and Stress Analysis
4.7 Vibration and Noise Control in Rotors
4.8 Simulation and Optimization of SC-VTOL Rotor Design
4.9 Testing and Validation Methodologies
4.40 Integrating the Rotor into the Overall SC-VTOL Design
5.5 eVTOL and UAM: Electric Propulsion, Multiple Rotors
5.5 Emerging Certification Requirements (SC-VTOL, Special Conditions)
5.3 Energy and Thermal in E-Propulsion (Batteries/Inverters)
5.4 Design for Maintainability and Modular Swaps
5.5 LCA/LCC in Rotorcraft and eVTOL (Footprint and Cost)
5.6 Operations & Vertiports: Airspace Integration
5.7 Data & Digital Thread: MBSE/PLM for Change Control
5.8 Tech Risk and Readiness: TRL/CRL/SRL
5.9 IP, Certifications, and Time-to-Market
5.50 Case Clinic: Go/No-Go with Risk Matrix
6.6 eVTOL and UAM: Electric Propulsion, Multiple Rotors
6.2 Emerging Certification Requirements (SC-VTOL, Special Conditions)
6.3 Energy and Thermal in E-Propulsion (Batteries/Inverters)
6.4 Design for Maintainability and Modular Swaps
6.5 LCA/LCC in Rotorcraft and eVTOL (Footprint and Cost)
6.6 Operations & Vertiports: Airspace Integration
6.7 Data & Digital Thread: MBSE/PLM for Change Control
6.8 Tech Risk and Readiness: TRL/CRL/SRL
6.9 IP, Certifications, and Time-to-Market
6.60 Case Clinic: Go/No-Go with Risk Matrix
- Hands-on methodology: test-before-you-trust, design reviews, failure analysis, compliance evidence.
- Software (depending on licenses/partners): MATLAB/Simulink, Python (NumPy/SciPy), OpenVSP, SU2/OpenFOAM, Nastran/Abaqus, AMESim/Modelica, acoustics tools, planning toolchains DO-178C.
- SEIUM Laboratories: scale rotor bench, vibrations/acoustics, EMC/Lightning pre-compliance, HIL/SIL for AFCS, data acquisition with strain gauging.
- Standards and compliance: EN 9100, 17025, ISO 27001, GDPR.
Capstone-type projects
Admissions, fees, and scholarships
- Profile: Background in Computer Engineering, Mathematics, Statistics, or related fields; practical experience in NLP and valued information retrieval systems.
- Documentation: Updated CV, academic transcript, SOP/statement of purpose, project examples or code (optional).
- Process: Application → Technical evaluation of profile and experience → Technical interview → Review of case studies → Final decision → Enrollment.
- Fees:
- Single payment: 10% discount.
- Payment in 3 installments: No fees; 30% upon registration + 2 equal monthly payments of the remaining 35%.
Monthly payment: available with a 7% commission on the total; annual review.
Scholarships: based on academic merit, financial need, and promoting inclusion; agreements with companies in the sector for partial or full scholarships.
See “Calendar & Calls for Applications,” “Scholarships & Grants,” and “Fees & Financing” in the SEIUM mega-menu.
Do you have any questions?
Our team is ready to help you. Contact us, and we will respond as soon as possible.
F. A. Q
Frequently asked questions
Yes, we have international certification
Yes: experimental models, real data, applied simulations, professional environments, real case studies.
It is not mandatory. We offer leveling tracks and tutoring.
Completely. It covers e-propulsion, integration, and emerging regulations (SC-VTOL).
Recommended. There are also internal challenges and consortiums.
Yes. Online/hybrid modality with planned labs and visa support (see “Visa & Residence”).