Potable Water Unit Low Temperature

AP 2000DB – AP 3000DB – AP 3600DB

The potable water units are designed to supply potable water to aircraft according to the highest standards in terms of safety, reliability and hygiene. These models are specifically set up to operate perfectly at low temperatures. Built on a sturdy steel chassis, they are equipped with a closed cab on the left-hand side of the frame, an insulated canopy for the systems 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 powered by a Perkins 404D-22 diesel engine 36.3 kW/49 bhp @2800 rpm positioned on the right-hand side of the frame. Hydrostatic transmission. 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. ssima di sollevamento di 1800 mm or 3000 mm, the platform can be equipped with anti-collision sensors (ultrasonic and/or antennas).

The vehicle is powered by a Perkins 404D-22 diesel engine 37.3 kW/50 bhp @2800 rpm positioned on the right-hand side of the frame. Hydrostatic transmission. 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.

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