Aircraft > Multi-Engine Piston > Tecnam > N386US: Tecnam P2006T Very Light Twin
GDU 1050 10-inches PFD GDU 1054 10-inches MFD Dual GEA 71B Engine & Airframe unit Dual GIA 64WAAS Com/nav/GPS/GS/Loc GMA1360 Digital audio system GMU44 Magnetometer GDC72 Air data computer GRS79 AHRS GTP59 OAT GTX345R Mode S Transponder (ADS-B In and OUT) S-TEC 55 dual Axis Autopilot with Electric Trim
Max Cruise Speed KTAS 269 km/h 145 kts Stall Speed (Flaps Down Power Off) KCAS 102 km/h 55 kts Max Operating Altitude 4.267 m 14.000 ft Take off run 301 m 988 ft Take off distance 394 m 1.293 ft Rate of climb 5,3 m/sec 1.036 ft/min Landing Run 231 m 758 ft Landing Distance 349 m 1.145 ft Range 1.204 km 650 nm
Engines – 2 Rotax 912S3 100 Hp, 4 Cylinders Liquid/Air Cooled, Integrated Reduction Gear Dual Ignition System Throttle Control LH/RH Tubular Steel Engine Mount Propellers – 2 MT, 2 Blades, Constant Speed, Full Feathering Propeller Spinner, Two Propeller Control LH/RH Air Filter, Two Oil Filter, Two Oil and Water Coolers, Two Carburettor Heat with Manual Control
Avionics Instruments Internally Lighted Avionics Radios Internally Lighted Engine Instruments Internally Lighted Flight Instruments Internally Lighted Compass Internally Lighted Map Light Dimmers Windshield Defroster Ventilator adjustable, 4 Place Heating System Epoxy Corrosion Proofing, All Structure LH Front Door Pilot/Co-Pilot, Lock and Key RH Rear Door Passenger Rear Window All Windows Tinted Retractable Landing Gear Tie Down Rings Main Wheels, 6.00 X 6 – Nose 5,00 X 5 Nav. Lights LED with Strobe Full LED TSO Vertical Tail Strobe Landing/Taxi Light LED