Aircraft Loads

This area of our activities comprises aircraft loads calculations and analysis per applicable airworthiness regulations, specifically -

• Flight Loads (including Flight Envelope / V-n Diagram development)

• 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.

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