Equipment Details Manufacturer: Honeywell Aerospace Model: T55-L-712 Equipment Type: Aircraft Turboshaft Engine Serial Number: LE-79144C Fuel Type: Jet A Maximum Recorded Test Data Power Output: 3,676.24 hp N1 Speed: 102.81% N2 Speed: 98.96% Torque: 1,272.29 ft-lb Measured Gas Temperature: 1,475.33°F Average Fuel Flow: 1,930.46 lb/hr Calculated Fuel Flow: 4.76 gal/min Compressor-Discharge Pressure: 105.63 PSI Compressor-Discharge Temperature: 630.38°F Main-Oil Pressure: 118.30 PSI No. 2 Bearing Pressure: 63.43 PSI Power-Turbine Bearing Pressure: 79.50 PSI Oil Temperature: 175.79°F Fuel Temperature: 80.71°F Recorded Vibration Data Maximum-power vibration readings documented on the primary run sheet: Compressor Vibration: 0.05 Axial Vibration: 0.56 Power-Turbine Vibration: 0.31 Additional documented test displays include: 2,430 hp Test Point: N1 95%, N2 96%, MGT 1,232°F, main-oil pressure 119 PSI, and vibration readings of 0.04 inlet, 0.47 axial, and 0.23 power turbine 2,101 hp Test Point: N1 93%, N2 100%, MGT 1,184°F, main-oil pressure 120 PSI, and vibration readings of 0.05 inlet, 0.49 axial, and 0.24 power turbine Pricing, mileage and/or engine hours are approximate and subject to change. Equipment specifications, battery condition, configuration, included components, operating condition, and availability are subject to verification. Please contact your sales representative for the most current information.