TPE331-10 TURBOPROP ENGINE Advanced engine performance and power generation capability Basic Engine Includes • Control System - Single Red Line /Auto-Start Controller 1100 • Fuel Pump • Fuel Anti-ice Heating System • Dual Continuous Ignition System • Lubrication System • Propeller-Pitch Control • Oil Temperature-Sensing Bulb • Negative-Torque-Sensing (NTS) System • Beta-Pressure Sensing Switch • Fuel Shutoff Valve • Torque and Temperature Limiting • Fuel Purge System • Fire-Shield Adapter • Propeller Flange TRUE AIRSPEED, V-KNOTS • Air Speed and Ambient Pressure Ratio Transducer Optional Accessories/Features Starter or Starter Generator Aircraft Accessories • Water Methanol Augmentation Manifold • Aluminum Gearbox High performance, increased performance and lower cost of ownership Propeller Governor Prop Pitch Control Tachometer Generator FUEL FLOW (WF) LB/HR • Propeller Governor

TPE331-10 Turboprop Engine Specifications (Sea level-standard day) Power output: shp shp (thermo) eshp eshp (thermo) Pressure ratio: (Demonstrated) Start capability: 41,730 2,000 (cw from rear) 1,591 (ccw from rear) FUEL CONTROL REAR MOUNT FUEL MANIFOLDS (Demonstrated) SL–45,000 ft. No minimum O.A.T to + Operational limits: 55ºC REAR MOUNT STARTING FUEL MANIFOLD Compressor bleed: high pressure 10% (max) ACCESSORY CASE AIRCRAFT ACCESSORY TYPE OF DRIVE (ONE EACH) ROTATION FACING DRIVE PAD AND RPM AND20002 RPM, T ,T , AND c o CCW STARTER-GENERATOR TYPE X11-D STUD PATTERN 10,887 OR ALTERNATOR (MODIFIED)...