News & Blog

Zero-click Loadsheet

We launched cooperation with Wizz Air three years ago, promising a Loadsheet procured in less than 60 seconds. We achieved that by building a software solution with a User Interface (eXperience) fully aligned to the airline’s Ground Handling procedure—a simple, even simplistic interface requiring minimum interactions. But optimizing human interactions can only go so far. Every consecutive change brought limited return—it would not decrease the time further. The next step was connecting systems that could provide data to the “calculator” (e.g., DCS, flight schedule, EFB), eliminating redundant data input completely.  

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Structural Limitations: Maximum Running Loads

Running load is a limitation that prevents floor damage.

It is given as kilogram per meter, kilogram per inch, or pound per inch. And 62 kg/in limit means that if we cut the aircraft fuselage in slices (the width of each is 1 inch) the total mass loaded in the slice cannot exceed 62 kg. The limit can be set differently in different areas of the aircraft. Usually, it is higher in the section over the wing and decreases in the AFT part of the aircraft.

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The role of the flight instructor in pilot training

Each pilot perfectly remembers his first flight and the instructor who introduced him to the world of aviation. With this instructor, we took our first steps in the sky and under his watchful eye we felt what it was like to “break away from the ground”.

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Structural Limitations: Accumulated Loads

The aircraft structure is designed to withstand certain bending moments and vibrations. To prevent excessive forces exerted on a structure, manufacturers regulate the weight of the load that is allowed in a given section of a fuselage. The limitation can apply to the whole hold space or only some designated part of it.

In the Evionica’s Weight and Balance solution, the fuselage section can be arbitrarily defined together with a weight limitation that should be validated.

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