"DESIGNED FOR THERMAL OXIDATION STABILITY TESTING OF AVIATION TURBINE FULES; 100 - 380 C TEST TEMP; 0 - 300 MM HG PRESSURE DIFFERENTIAL; 500 PSI SYSTEM PRESSURE; LARGE LCD TOUCH SCREEN; RS-232 USB (2) INTERFACES; 115V, 8A OR 230V, 4A; 47 - 63 HZ; LESS THAN 600 MLS NEEDED FOR TESTING SAMPLE; POUR-AND-GO OPERATION; AUTOMATIC AERATION AND FUEL CLEANING AT BEGINNING OF TESTING"