This area of our activities comprises aircraft loads calculations and analysis per applicable airworthiness regulations, specifically -
• Control Surface and System Loads
• Stabilizing and Balancing Surfaces Loads
• Ground Loads
• Water Loads
• Emergency Landing Loads
• Load Report Generation and Substantiation
The aircraft loads will be defined according to airworthiness regulations as applicable to the project, for instance:
• FAR Part 23
• EASA CS-23,
• US LSA Rules (ASTM specification F2245),
• EASA CS-VLA,
• German LTF-UL.
Load reports can be used at later stages of the project for structural testing, as well as indispensable part of compliance documentation for the certification process, if applicable.