The objective of the training is to enable participants to understand power input quality and electromagnetic compatibility (EMC) requirements within the scope of aviation standards, including MIL-STD-461, DO-160, and MIL-STD-704. The program also aims to enhance participants' competencies in analog design by enabling them to learn the design principles of analog filtering and protection circuits used to achieve compliance with these standards through practical application examples.

• Power Input Quality
• MIL-STD-704 Requirements
• RTCA DO-160 Requirements
• Power Input Quality Practices
• Low Voltage Transients
• High Voltage Transients
• Electromagnetic Compatibility (EMC)
• MIL-STD-461 Requirements
• RTCA DO-160 Requirements
• EMC Applications
• Power Input EMI Filtering
• Signal Interface EMI Filtering
• Lightning Protection
• Grounding

• Participants will be able to explain key aviation standards such as MIL-STD-461, RTCA DO-160, and MIL-STD-704.
• Participants will be able to develop analog design solutions that meet the requirements of key aviation standards such as MIL-STD-461, RTCA DO-160, and MIL-STD-704.
• Participants will be able to acquire a troubleshoot perspective on issues that may arise during EMI/EMC compliance testing processes.

There are no prerequisites for this training.

The training is primarily intended for hardware design engineers.

The training will be conducted theoretically in a classroom setting arranged like a meeting or briefing room, using a whiteboard, projector, computer, and MS Office tools.

The objective of this training is to provide current and essential knowledge within the framework of avionics digital electronic design processes. It covers topics such as the certification of electronic boards, avionics design architectures, avionics electrical interfaces, high-speed data bus design, component management, and the pre-validation and troubleshooting of electronic boards.

• Digital Electronic Design in Avionics
• Digital Electronic Design and Certification
• Avionics Design Architectures
• Component Selection and Management
• Avionics Digital Interfaces
• High-speed Data Bus Design
• Electronic Board Pre-validation and Troubleshooting

• Participants will be able to identify design and certification processes in avionics systems.
• Participants will be able to explain avionics design architectures.
• Participants will be able to apply material selection and component management processes.
• Participants will be able to design and evaluate avionics digital interfaces.
• Participants will be able to apply design and simulation methods for high-speed data buses.
• Participants will be able to apply pre-validation and troubleshooting methods for electronic circuit boards.

Participants are expected to have prior knowledge of fundamental concepts in digital electronics design and hardware development processes.

The training is primarily intended for hardware design engineers.

The training will be conducted theoretically in a classroom setting arranged like a meeting or briefing room, using a whiteboard, projector, computer, and MS Office tools.

The objective of this training is to address the role of FPGA design within avionics systems from a system, process, and safety perspective. The course establishes foundational awareness among participants of the distinctions in FPGA design for avionics projects, the requirements-based design approach, and certification considerations. Apart from providing deep technical instruction, the training aims to help participants understand the bigger picture and develop the ability to ask the right questions.

• FPGA Design in Avionics
• Fundamental Concepts in FPGA Design
• Usage of FPGA in Avionics Systems
• FPGA Design Process and Certification
• Requirements-Based FPGA Design
• Safety and Coding Perspective
• Pre-Verification and Debugging in FPGA Design

• Participants will be able to describe the use of FPGAs in avionics systems.
• Participants will be able to explain the importance of certification and process discipline in avionics projects.
• Participants will be able to define the significance of a requirements-based design approach.
• Participants will be able to illustrate the impact of the DO-254 framework on FPGA design.
• Participants will be able to explain the importance of coding from a safety and security perspective.

Participants are expected to have prior knowledge of fundamental FPGA and digital design concepts, as well as hardware development processes.

The training is intended for digital design engineers.

The training will be conducted in a classroom setting through presentations and will employ conceptual explanations, sharing of real project experiences from an avionics systems perspective, discussion sessions based on example scenarios, as well as interactive Q&A and evaluation methods.

The objective of this training is to provide a comprehensive understanding of the mechanical design process and fundamental industrial design principles for avionic LRU systems, tailored to specific system requirements. Additionally, it seeks to develop knowledge in key areas, including dynamic and static testing and verification, analysis, shock and vibration considerations, material selection, and sealing techniques, ensuring compatibility with environmental conditions.

• Avionics LRU Mechanical Design Process and Basic Industrial Design Concepts
• Environmental Conditions and Avionics LRU Mechanical Design Steps
• Sealing, Material Selection
• Vibration, Shock, Static and Dynamic Test/Verification and Analysis Concepts

• Participants will be able to describe the mechanical design processes of avionic LRUs and fundamental industrial design principles.
• Participants will be able to explain material selection and sealing techniques in compliance with environmental conditions.
• Participants will be able to define the basic concepts of shock, vibration, static and dynamic testing/verification, and analysis.

There are no prerequisites for this training.

The training is intended for mechanical design engineers.

The training will be conducted theoretically in a classroom environment arranged in the style of a meeting or briefing room, using a whiteboard, projector, computer, and MS Office tools.

The objective of this training is to offer an in-depth understanding of the mechanical design process and fundamental industrial design principles in Inertial Navigation Systems, grounded in specific system requirements. Furthermore, it seeks to enhance knowledge in critical areas, including dynamic and static testing and verification, analytical methods, shock and vibration considerations, material selection, and sealing techniques, ensuring alignment with environmental conditions.

• Mechanical Design Process of Inertial Navigation Systems and Basic Industrial Design Concepts
• Environmental Conditions and Mechanical Design Steps of Inertial Navigation/Measurement Systems
• Sealing, Material Selection
• Vibration, Shock, Static and Dynamic Test/Verification and Analysis Concepts

• Participants will be able to explain the mechanical design processes and fundamental industrial design principles of Inertial Navigation Systems.
• Participants will be able to describe material selection and sealing techniques in compliance with environmental conditions.
• Participants will be able to define the basic concepts of shock, vibration, static and dynamic testing/verification, and analysis.

There are no prerequisites for this training.

The training is designed for mechanical design engineers.

The training will be conducted theoretically in a classroom environment arranged in the style of a meeting or briefing room, using a whiteboard, projector, computer, and MS Office tools.

The objective of this training is to provide a comprehensive understanding of the thermal design of avionic units capable of operating under extreme temperature conditions, in accordance with MIL-STD-810 and DO-160G standards.

• Military Standards and Definitions; General Overview of Active and Passive Thermal Design Applications
• Thermal Modelling with CFD (Computational Fluid Dynamics) Analyses
• Modelling Levels in Thermal Design
• Supporting CFD Analyses Through Test and Measurement Activities
• Overview of Applicability for Emerging Technologies in Thermal Design

• Participants will be able to define the thermal design methods and process details at various modelling levels in avionic units.

Participants are expected to have basic knowledge of thermodynamics, heat transfer, and fluid mechanics.

The training is intended for mechanical design engineers.

The training will be conducted theoretically in a classroom environment arranged in the style of a meeting or briefing room, using a whiteboard, projector, computer, and MS Office tools, with real-life examples presented as supporting materials.

The objective of this training is to provide insight into the fluid dynamics simulations and test activities employed in the mechanical design of avionic subsystems. Furthermore, it seeks to familiarise participants with standards related to fluid dynamics applications and to illustrate design verification through relevant case studies.

• Basic Concepts Related with Fluid Dynamics
• Fluid Dynamics Applications Utilized in Mechanical Design
• Standards Related with Fluid Dynamics and Aerodynamic Design
• Case Studies of Design Verification Tests and Simulations

• Participants will be able to assess the design requirements related to fluid dynamics in avionic units.
• Participants will be able to define the fundamental concepts and approaches of fluid dynamics.

Participants are expected to have basic knowledge of fluid dynamics, aerodynamics and thermodynamics.

The training is designed for mechanical design engineers.

The training will be conducted theoretically in a classroom environment arranged in the style of a meeting or briefing room, using a whiteboard, projector, computer, and MS Office tools.

The objective of this training is to provide participants with a comprehensive understanding of the fundamental concepts of avionics software development, the DO-178C lifecycle, and the associated certification procedures. Furthermore, the course seeks to highlight the distinctions between software development within the avionics domain and conventional software engineering practices.

• Introduction and Basic Concepts
• DO-178C and Software Lifecycle
• Avionics Software Development
• Avionics Software Verification
• Software Configuration Management
• Software Certification
• Q&A

• Participants will explain avionics systems and software concepts, recognising the challenges inherent in this field. Participants will also become familiar with DO-178C-compliant development, verification, configuration, and certification processes, and will be able to articulate how they can advance their own skills in these areas.

Participants are expected to have basic knowledge of software development processes and lifecycles.

The training is designed for software design engineers.

The training will be conducted in a classroom setting through presentations and will employ conceptual explanations, sharing of real project experiences from an avionics systems perspective, discussion sessions based on example scenarios, as well as interactive Q&A and evaluation methods.

The objective of this training is to provide participants with knowledge of driver software architectures developed for operating systems used in avionics software design.

• Processor Board Bring Up
• Avionics Communication Interfaces
• Driver Software Architectures
• Memory Mapped Driver Development
• I/O Driver Development

• Participants will be able to bring up a newly introduced processor board and prepare it for use with the required avionics communication interfaces.

There are no prerequisites for this training.

The training is designed for software design engineers.

The training will be conducted theoretically in a classroom environment arranged in the style of a meeting or briefing room, using a whiteboard, projector, computer, and MS Office tools.

The objective of this training is to enable participants to gain a general understanding of avionics systems used in aircraft, including their historical development, components, and development and qualification processes.

• Introduction To and History of Avionics Systems
• Human Machine Interface Systems
• State Sensors
• Navigation Systems
• External World Sensors
• Mission Systems
• Avionics Architectures
• Avionics System Development Process
• Qualification / Certification Process

• Participants will be able to identify avionics system components.
• Participants will be able to explain the functions of these components.
• Participants will be able to describe the development and testing processes of avionics systems.
• Participants will be able to establish a common terminology by defining the interaction and interoperability of system components.

There are no prerequisites for this training.

The training is designed for avionics systems design engineers.

The training will be conducted theoretically in a classroom environment arranged in a meeting or briefing room format, using a whiteboard, projector, computer, MS Office tools, and both fictional and real-life examples.

The Flight Management System (FMS) is a software system that automates and facilitates many calculations and functions related to flight planning and navigation. The objective of this training is to provide participants with fundamental knowledge of the FMS, one of the most critical components of modern aircraft.

• What is FMS?
• FMS Functions
• Position Determination
• Flight Planning
• Autopilot Interface and Guidance
• Indications and Warnings
• FMS Manufacturers
• FMS in the Future

• Participants will be able to describe the general concepts related to the FMS.
• Participants will be able to identify the functions within the scope of the FMS.
• Participants will be able to explain the basic concepts of navigation sensors.
• Participants will be able to define the fundamental concepts related to flight control points and flight plan creation.
• Participants will be able to explain the importance of using aircraft performance data.
• Participants will be able to generate the data required for FMS autopilot integration.
• Participants will be able to examine and interpret the alerts and notifications associated with the FMS.
• Participants will be able to develop an understanding of the evolution and future of the FMS.

There are no prerequisites for this training.

The training is designed for avionics system design engineers and avionics software design engineers.

The training will be conducted theoretically in a classroom environment arranged in a meeting or briefing room format, using a whiteboard, projector, computer, MS Office tools, and both fictional and real-life examples.

The objective of this training is to enhance participants' understanding of the processes followed in modernization projects for rotary-wing platforms. It aims to provide a holistic, platform-level perspective by presenting information on the placement of sub-disciplines--each representing a distinct area of expertise--within the aircraft, their interconnections, and the precedence or sequential relationships that integrate them.

• Offer Process
• System Design Process
• Integration Process
• ILS Process

• Participants will be able to describe the modernization process of a rotary-wing platform.
• Participants will be able to explain how activities from different disciplines are integrated on the platform and their interrelationships.

Participants are expected to have basic knowledge of aviation.

The training is designed for avionics system design engineers.

The training will be conducted theoretically in a classroom environment arranged in a meeting or briefing room format, using a whiteboard, projector, computer, MS Office tools, and both fictional and real-life examples.

The objective of this training is to enhance participants' knowledge of applying the Avionics System Safety Engineering approach in product development projects. It covers topics implemented throughout the product development process, including functional hazard analysis, fault tree analysis, design assurance, and system safety assessment, and aims to provide detailed information on the relevant standards and manuals.

• What is Safety?
• Certification and Safety
• Failure Conditions
• Functional Hazard
• Preliminary System Safety Assessments
• Fault Trees
• Design/Development Assurance Level
• Common Mode and Intrinsic Hazard Analysis
• System Safety Assessment
• FFPA
• Avionics System Safety

• Participants will be able to explain the application of the avionics system safety engineering approach in product development projects.
• Participants will be able to evaluate functional hazard analysis, fault tree analysis, design assurance, and system safety throughout the product development process.

Participants are expected to have basic knowledge of aviation.

The training is designed for special engineering teams.

The training will be conducted theoretically in a classroom environment arranged in a meeting or briefing room format, using a whiteboard, projector, computer, MS Office tools, and both fictional and real-life examples.