Project brief
Complete technical report package supporting a type certification application for a commercial 25kg fixed-wing UAV under EASA Special Condition SC-RPAS-01. The package covers airworthiness substantiation across 14 technical disciplines, supporting the design organization approval (DOA) submission and demonstrating compliance with EASA CS-RPAS requirements for commercial BVLOS operations.
The supplied record concerns support for an application, not a new approval granted by this portfolio. The enrichment preserves that distinction.
The engineering challenge
Assemble multidisciplinary UAV engineering evidence into a coherent certification-support narrative.
Engineering approach
- Organize structures, propulsion, avionics, software, and operational evidence.
- Connect analysis and flight-test material to the report's technical scope.
- Consolidate link, detect-and-avoid, and risk-assessment references for review.
Features & capabilities
- Airworthiness substantiation: structures, propulsion, avionics, software, EMC
- Flight performance: cruise, climb, glide, stall, control margins
- Structural analysis: FEA of composite airframe, wing, tail, landing gear
- Flight test report: 240 flight test sorties, 180 flight hours of data
- Ground proximity sensor qualification and obstacle avoidance testing
- Detect and Avoid (DAA) system capability report for BVLOS operations
- Command and Control link analysis: link budget, coverage, encryption
- Operational risk assessment (SORA): ConOps, ARC, SAIL determination
Software & engineering tools
ANSYS Mechanical FEA, MATLAB flight performance model, technical writing per EASA AMC/GM, AC-91 UAV