Our Systems Engineering services help structure large, multi-system programs in accordance with ARP-4754B, defining architectures, interfaces, and development assurance levels across avionics, flight control, propulsion systems or any complex safety critical system. For example, we have supported programs involving integrated modular avionics (IMA) and electrically powered flight control actuation, where clear system architecture and requirement traceability were critical for compliance and coordination between OEMs and Tier-1 suppliers.

Through Safety & Reliability Engineering, we ensure that complex systems—from digital flight control computers to engine management and power distribution—meet certification objectives under ARP-4761A. We develop safety artifacts such as FHA, PSSA, SSA, and CCA, and perform quantitative analyses using Fault Tree Analysis (FTA) to support compliance with EASA CS-25.1309. This provides clear evidence that system architectures achieve both reliability and safety objectives.

Our Software Development experts help integrate high-criticality applications developed under DO-178C / ED-12C, supporting software planning, tool qualification, and verification. We can act as Software CVEs, perform independent audits, or assist with Stage of Involvement (SOI) preparation to ensure smooth certification with authorities. Whether developing flight control or engine control software, IDA ensures that development assurance and verification activities align seamlessly with system and safety requirements.

Finally, Product Security has become a key element in large aircraft development. We apply ED-202B / DO-326B, ED-203A / DO-356A, and ED-204A / DO-355 standards to ensure that cyber resilience and continued airworthiness are integrated into both airborne and ground systems. For example, we perform Security Risk Assessments (SRA) for avionics networks and prepare Plans for Security Aspects of Certification (PSecAC) to support compliance with EASA AMC 20-42.