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
+49 179 322 4970
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
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Chief of the Office of Airworthiness at EASA Part 21J approved DOA, Germany
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Compliance Verification Engineer (CVE) for Cabin Safety & Structure, Germany
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Quality Assurance Post Holder at UAE GCAA CAR 147 approved Training Organisation, Dubai
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Technical Project Manager & System Engineer of MA700 Cabin Pressure Control System, Germany
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Lecturer & Trainer, Germany
Qualification
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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
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Diplom-Ingenieur, Aerospace Engineering at the University of Stuttgart
Modelling of a system management for a safety critical fly-by-wire platform