- Made on trailing 4-wheeled cart basis, electroplated with h/z and with galvanic coating;
- Wheels - pneumatic 4.00-8;
2 tanks
a)for refueling the aircraft with drinking water of 800 liters;
b)for draining drinking water from the substation 200 l;
- On-board volume measuring unit to measure drinking water poured into the aircraft;
- The tank for filling of PS with drinking water is made of food stainless steel;
- Draining drinking water tank is made from stainless steel;
- the pump with a productivity not less than 70 l / min . and not less than 1.8 bar;
- possibility of shutdown of the pump at the working engine by the distributing device;
- hosepipe with connector length not less than 5 m and a diameter of not less than 25 mm;
- the availability of the universal adapter for connect hoses to the respective systems of the aircraft;
- sensor of the water degree;
- technical hatch for access to the inside of the tank;
- filling nozzle for filling by hydrant;
- winter package with installation complete insulation of the tank and autonomous gasoline heating system, similar Webasto or Eberspacher for use when the external temperature to - 20 C;
- Battery not less than 60 A/h;
- stationary charging device for charging the battery installed ;
- system heating of water, mode use in electrical network 220V;
- the wire to connect to the electricity network 220V length not less than 5 m;
- the chassis are equipped with the mechanical parking brakes, which work at lifting of a carrier, providing reliable fixing of installation during parking;
- flashing beacon;
- interior lighting of technical compartments for work at night;
- external lighting for work at night time;