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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.

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.

Cargo operations are usually challenging. In many cases, they require the loadmaster to travel with the aircraft to supervise the loading and offloading process. Is it...

Have you ever wondered how we know the final mass of the aircraft? It’s calculated in the Weight and Balance process by correcting aircraft empty mass with CREW, FUEL,...

Cargo movement would result in an uncontrolled Center of Gravity shift during flight. That is why every Unit Load Device (pallet or container) must be secured to stay...

When creating a Loadsheet document using Evionica Weight and Balance software, on the “Loadsheet” step one can choose between the Final and Preliminary designation of...

Discover all of the Weight and Balance solutions for cargo airline, passenger airline and ground handling provided by Evionica. Meet us at Booth #E61 during 23rd GHI conference and let’s talk about the smartest solution for your airline.
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