These models of Potable Water Units are all designed to ensure an efficient supply of potable water to all the types of aircrafts, according to high security standards, reliabi-lity and hygienic conditions. These models are characterized by the presence of a PLC control which manages all the machine functions and the security as well.
WATER CIRCUIT
• - Water tank made in AISI 304 stainless stoel. 3 mm thickness, manhole 0 500 mm
• - Centrifugal transfer pump. flow rate 90 l/min
• - Pressure control
• - Liters counter with predctermination and calculation of quantity in the tank
• - Flexible hose for low pressure with a aircraft standard connection
• - Sphere valve 1" 1/2 for the total discharge of the tank
• - Plastic housmg filter with stainless steel cartridge 70 p.
ENGINE
• - 404D-22 PERKINS water cooled engine. power 37.3 kW/50 bhp @28C0 rpm 4 cylin-
der 2.2 litre unit, émissions législation for EC Stage IIIB/USA EPA Tier 4
• - D 2011 L3 i - DEUTZ air/oil ccoled engine. power 36.3 kW/49 bhp @2800 rpm 3
cylinder 2.33 litre unit, émissions législation for EC Stage IIIA/USA EPA Tier 3
• - 4LE1 ISUZU water cooled engine. pcwer 36 kW/48 bhp @2600 rpm 4 cylinder 2.2
litre unit, émissions législation for EC Stage III Alnterim Tier 4
WINTER KITS (Optional)
• - Warm-up winter kit 220V -40° (engine heater. battery charger, cabin heater. cabinet
heater).
• - Completely closed cabinet made on 40mm insulated panel over the tanks and
equipment.
• - WEBASTO heater under the canopy