Description/Function of unit The test stand is designed to provide a source of hydraulic power up to 34 GPM, at 3500 PSIG with open or closed loop operation and to service the aircraft reservoir using a low pressure fill system. The stand instrumentation includes pressure, flow and temperature display. The unit is completely self-contained and requires only connection to a source of 460 volt, 3 phase, 60 HZ. Note: 240 VAC, on request. Leading Particulars Test fluid:Skydrol Temperature:160º maximum shut down Filtration:Supply 3 micron absolute, Return 10 micron nominal, Fill 5 micron Electric power Input:460 volts, 3PH, 60Hz, 78 FLA Instrumentation
Supply pressure gauge, 0-6000 PSI, 6 dial Boost/return system gauge, 30 in HGA to 300 PSI, 4 dial Temperature gauge, 4ºF -200ºF, 3½ dial Flowmeter, 3-34 GPM Major Components Reservoir, stainless steel Boost pump, integral to main pump Main pump, variable volume, pressure comp. 0-34 GPM, 3500 PSI,5000 PSI at reduced flow Main pump/motor, 60Hp, 1750 RPM, 460V, 3PH, 60Hz Fill pump motor, ½ HP rating 460V, 3PH, 60 Hz Heat exchanger, air to oilApplicability All narrow body aircraft including A319 and A320 |