Ground Support Equipment

Mobile unit for testing of main and reserve hydraulic systems of an aircraft in airfield conditions.Aircraft and helicopter design. Two independent hydraulic circuits. Can be used for refueling systems.

Aircraft version:

• 35 MPa pressure
• Flow rate 125 l/min per circuit
• Working fluid Skydrol
• Power rating 90 kW
• Working Fluid Clarity 3 microns
• Air cooling
• Operating temperature range 0 … 50 °C

Helicopter version:

• Pressure 8 MPa
• Supply 40 l/min per circuit
• Operating-liquid AMG10
• Gas – nitrogen, cylinder 40 l, charging pressure 3 MPa

The test rig can be designed according to a simplified scheme directly connected to the airplane reservoir, without refueling. 

• 2 independent pressure circuits
• Pressure 15 MPa
• Working fluid FH51
• Supply 40 l/min per circuit
• Manual ergonomic control