The UAV Wing Load Testing Jig is a precision structural analysis platform purpose-built for verifying the integrity of UAV wings and airframe components under controlled static loading conditions. Employing the Whiffletree multi-point load distribution method, the system accurately replicates aerodynamic pressure profiles across full-scale or model-size UAV structures, eliminating the oversimplifications of single-point loading and providing results that directly reflect real-world flight loading scenarios.

The system integrates a 15-ton CNC-machined steel frame, high-accuracy strain gauges, LVDT displacement sensors, load cells, and inclinometers into a unified 24-bit data acquisition and analysis workflow. Compliance with EASA and FAA structural testing standards makes the UAV-Lab 500 suitable for both certification campaigns and research programs, while its modular frame and detachable clamping fixtures allow rapid reconfiguration across different UAV geometries and test setups.