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Training / Education

DO-178C Basic Training

This course is offered in China only and presented in Mandarin Chinese. The course materials are bilingual (English and Chinese). This course is offered in Mandarin Chinese. The course materials are in English and Chinese. RTCA DO-178C is the accepted standard for civil aviation software development and certification, and Chinese civil aviation companies must comply with this standard to meet airworthiness requirements. Participants will attain a basic understanding of the concepts of DO-178C and how it is properly utilized.

Training / Education

Design Verification Plan & Report (DVP&R) - Overview and Application

This course is verified by Probitas as meeting the AS9104/3A requirements for Continuing Professional Development. In this one-day course on Design Verification Plan and Report Overview and Application, participants will be introduced to important concepts, the basic theory behind the concepts, and discuss how these concepts can be applied to the client's design reliability activities. Participant involvement will be maximized to demonstrate and reinforce the concepts through reading assignments, group discussions, and exercises where students will begin a DVP&R on a client product.

Training / Education

Key Considerations for the Comparison of Power‐by‐Wire and Hydraulically Supplied Solutions for Aerospace Actuation

This four-hour short course provides key considerations for the comparison of electrically supplied (Power-by-Wire, or PbW) and hydraulically supplied (Power-by-Pipe, of PbP) actuation for aerospace. The focus is put on the consequence, for designers, of changing the physical principles and the technology used. A particular attention is paid to the unavoidable side effects introduced by the technological realization. Simple examples with realistic numerical values are used to make the comparisons quantitatively realistic.

Training / Education

Design Considerations for Electromechanical Flight Control Actuation Systems

This four-hour short course intends to present an overview of electrically powered flight control actuation systems, covering commercial applications. The scope covers issues related to the mechanical design of actuators themselves, with limited reference to their control electronics. Additionally, this course will provide participants an understanding of the design considerations behind these actuation systems.

Training / Education

DFMEA Overview and Application

During this DFMEA Overview and Application course, participants will be introduced to important FMEA concepts, the basic theory behind the concepts, then discuss how these concepts can be applied to the customer's design FMEA activities. Participant activities include: reading assignments, group discussions, exercises, building Block Diagrams as a group, and beginning a DFMEA on a customer’s product.

Training / Education

Problem Solving and Root Cause Analysis

This course is verified by Probitas as meeting the AS9104/3A requirements for Continuing Professional Development. Problems arise in all facets of life. This is particularly true in the business world. Problems impact all aspects of an organization’s operations such as; product development, product quality, process efficiency, marketing efforts, human relations, leadership efforts, financial execution and ultimate profitability. If these problems are not addressed, they inhibit the operation of the business and can eventually result in total failure.

Training / Education

DO-178C Practical Training

This course is offered in China only and presented in Mandarin Chinese. The course materials are bilingual (English and Chinese). RTCA DO-178C  is the globally-accepted standard for civil aviation software development and certification. Compliance with the objectives of DO-178C is the primary means for meeting airworthiness requirements and obtaining approval of airborne software in TC/STC/TSO, etc. Even after study of the DO-178C, many people lack experience producing DO-178C compliant airborne software in real applications.

Training / Education

Aviation Safety Engineer Job Functions

This course content provides the Civil Aviation Safety Engineers (Systems - Electrical) with the knowledge and skills to conduct oversight of aviation safety, aircraft certification and Continued Operational Safety. These areas of responsibility include, but are not limited to, Type Certification, Amended Type Certification, Supplemental Type Certification, Parts Manufacturing Approval (PMA), Technical Standard Order (TSO) Continued Operational Safety, Flight manuals, and Operational Approvals.

Training / Education

Design and Process Failure Modes and Effects Analysis (FMEA)

This course covers the five types of FMEAs with emphasis on constructing  Design and Process FMEAs. Each column of the FMEA document will be clearly explained using an actual FMEA example.  The course covers various methods for identifying failure modes, effects and causes with special attention given to severity, occurrence, and detection tables and how to develop effective recommended actions strategies.  Throughout the class, participants will be involved in exercises/actual projects that demonstrate and incorporate direct application of learned principles.

Training / Education

Guidance for Model-Based Development and Verification (DO-331)

This course is offered in China only and presented in Mandarin Chinese. The course materials are bilingual (English and Chinese). Model-Based Development and Verification (MBDV) technology has been widely accepted in software production. When this technology is used in airborne software, key issues should be considered to ensure airworthiness and safety goals are met. To facilitate the use the MBDV technology, RTCA DO-331 is published as a supplement and guidance support to DO-178C. Because MBDV is regularly used in critical software applications, guidance is needed to apply it to airborne software.

Training / Education

Fundamentals of Fatigue Analysis

Fatigue is a structural failure mode that must be recognized and understood to develop products that meet life cycle durability requirements. In the age of lightweighting, fatigue strength is an important vehicle design requirement as engineers struggle to meet stringent weight constraints without adversely impacting durability. This technical concept course introduces the fatigue failure mode and analysis methods. It explains the physics of material fatigue, including damage accumulation that may progress to product failure over time, and it provides the needed foundation to develop effective fatigue prediction capabilities.

Training / Education

Design Considerations for Hydraulically Powered Fly-By-Wire Flight Control Actuation Systems

This four-hour short course will present an overview of hydraulically powered flight control actuation systems used on fly-by-wire aircraft, covering both military and commercial applications. The scope this course covers the issues related to the mechanical design of actuators themselves, as well as their control electronics. Additionally, this course will provide participants an overview of the design considerations behind these flight control actuation systems.

Training / Education

Electrohydraulic Servovalves in Flight Control and Utility Actuators

This four-hour short course intends to present an overview of electrohydraulic flow control servovalves commonly used in flight control and utility actuators. The scope of this course covers the history and design of servovalves, as well as their most common performance characteristics. This course will provide participants an understanding of the application of electrohydraulic servovalves in hydraulically powered actuators and preparation of the servovalve procurement specification.

Training / Education

Design Considerations for Electrohydrostatic Actuators

This course is verified by Probitas Authentication as meeting the AS9104/3A requirements for continuing Professional Development. This four-hour short course will provide an overview of design considerations for electrohydrostatic actuation for transport and business aircraft applications.  The instructor will present the critical topics of electrohydrostatic actuation (EHA) from a systems development perspective (V-Approach).  Beginning with aircraft system requirements, the instructors will then guide participants through EHA subsystem requirements, component design, component verification test, aircraft integration, and use. 

Training / Education

Flight Control Actuation System Considerations on Architecture Design and System Installation

The purpose of this four hour short course is to provide information to understand how is established the basic architecture of a Flight Control Actuation System of a transport airplane, i.e. understanding the rationale for the distribution of the control surfaces, power sources, actuators and computers.

Training / Education

Applying DO-254 for Avionics Hardware Development and Certification

2024-11-20

This basic course introduces the intent of the DO-254 standard for commercial avionics hardware development. The content will cover many aspects of avionic hardware including, aircraft safety, systems, hardware planning, requirements, design, implementation, and testing. Participants will learn industry-best practices for real-world hardware development, common DO-254 mistakes and how to prevent them, and how to minimize risks and costs while maximizing hardware quality.

Training / Education

Introduction to DO-178C

2024-11-18

This two-day course will introduce participants to industry best practices for real-world software development and how to avoid common DO-178C mistakes. This course is intended to present the information necessary to help minimize DO-178C risks and costs, while also maximizing software quality during avionics development.  The instructor will guide participants through topics such as aircraft safety, systems, software planning, software requirements, and software design/code/test.  

Training / Education

Development and Practice of Airborne Electronic Hardware Based on DO-254

2024-08-27

This course is offered in China only and presented in Mandarin Chinese. The course materials are bilingual (English and Chinese). Participants in this course comprehensive understanding of the DO-254 standard including how the development of airborne electronic hardware (AEH) and the development of the aircraft system are related. It addresses the key objectives, activities, and generated data of the AEH lifecycle and presents common problems in the application of DO-254 and how to prevent them. This course also includes current AEH certification requirements and interprets some of the difficulties in gaining compliance approval.

Training / Education

DO-326A and ED-202A An Introduction to the New and Mandatory Aviation Cyber-Security Essentials

2024-07-29

This course will introduce participants to industry best practices for real-world aviation cyber-security risk-assessment, development & assurance. Participants will learn the information necessary to help minimize DO-326/ED-202-set compliance risks and costs, while also optimizing cyber-security levels for the development, deployment and in-service phases Topics such as aircraft security aspects of safety, systems-approach to security, security planning, the airworthiness security process, and security effectiveness assurance will be covered.

Training / Education

AS13100 and RM13004 Design and Process Failure Mode and Effects Analysis and Control Plans

2024-07-03

This course is verified by Probitas Authentication as meeting the AS9104/3A requirements for continuing Professional Development. In the Aerospace Industry there is a focus on Defect Prevention to ensure that quality goals are met. Failure Mode and Effects Analysis (PFMEA) and Control Plan activities are recognized as being one of the most effective, on the journey to Zero Defects. This two-day course is designed to explain the core tools of Design Failure Mode and Effects Analysis (DFMEA), Process Flow Diagrams, Process Failure Mode and Effects Analysis (PFMEA) and Control Plans as described in AS13100 and RM13004.