Services

Airworthiness &
Aircraft Certification

Civil aircraft design, certification, production, modification, operation, management or maintenance is subject to a very strict regulatory framework which is defined by the Civil Aviation Authority in the respective territory.

Development Process of
Aircraft Systems

Identifying and reducing design errors require a systematic development process that integrates the safety evaluation into the aircraft and system design process.

Safety Assessment of
Aircraft Systems

To assess the safety of an aircraft system, the safety effect needs to be evaluated and the method for how to conduct the safety assessment needs to be determined.

Fault-tolerant Systems


A safety-critical function requires a fault-tolerant platform on which it can be safely executed with high integrity and reliability.

Project Management

Achieving the project goal within a predefined time frame and budget is a something that needs to be well managed, specially when a certain level of quality needs to be maintained.

About me

Dr.-Ing. Mohamed Elmahdi

PhD graduated aerospace engineer with over 14 years of experience in design and certification of civil aircraft

Areas of expertise

– Initial Airworthiness (EASA Part 21, EASA CS25, Aircraft Design & Certification)
– Aircraft and System Development Process (ARP4754A)
– Aircraft and System Safety Assessment (ARP4761)
– Design principles of fault-tolerant control platforms
– Management of projects & qaulity

Work experience

Chief of the Office of Airworthiness at EASA Part 21J approved DOA, Germany

Compliance Verification Engineer (CVE) for Cabin Safety & Structure, Germany

Quality Assurance Post Holder at UAE GCAA CAR 147 approved Training Organisation, Dubai

Technical Project Manager & System Engineer of MA700 Cabin Pressure Control System, Germany

Lecturer & Trainer, Germany

Qualification

Doctor of Engineering Sciences, Aerospace Engineering, Institute of Aircraft Systems at the University of Stuttgart

Distributed Architecture of an IMA-based High Lift Control System

Diplom-Ingenieur, Aerospace Engineering at the University of Stuttgart

Modelling of a system management for a safety critical fly-by-wire platform