he potable water units are designed to supply potable water to aircraft according to the highest standards in terms of safety, reliability and hygiene. Built on a sturdy steel chassis, they are equipped with an open cab on the left-hand side and a 3 mm thick embossed finish stainless steel AISI 304 tank with a Ø 500 manhole and a 2″ ball valve for complete draining. Depending on the model, the load capacity ranges from 2000 to 3600 litres.
On the front right of the frame there is a platform which can be fixed or with a lift system with a maximum lifting height of 1800 mm or 3000 mm, the platform can be equipped with anti-collision sensors (ultrasonic and/or antennas).
The vehicle is equipped with a 240 Ah traction battery that powers the electric traction motor, the electric motor for the power steering, and the electric motor for the water pump. It has an automatic electric transmission and hydraulic power steering. The water system consists of a stainless steel transfer pump with a flow rate of 90/min, a digital litre counter with a preset automatic stop, a plastic filter with 70 μl stainless steel cartridge, a transfer pressure regulator, automatic backflow, and 4-metre long hose with standard aircraft coupling.