2026 2025 Tecnam P2010 in the US (N326UV)

Description

This 2025 Tecnam P2010 offers an almost-new opportunity, with exceptionally low flight hours, full IFR capability, and the comfort of a modern four-seat high-wing aircraft. Impeccably maintained and equipped for instrument operations from day one, it combines Garmin glass-cockpit technology with the simplicity, efficiency and reliability demanded by both private pilots and professional training fleets. Equally suited to upgrading a flight-school fleet or serving as a refined cross-country traveller, this P2010 delivers capability, comfort and operating confidence in a highly versatile platform.

Powerplant & Propulsion. At its heart is the proven Lycoming IO-390, delivering 215 HP at 2700 RPM through a fuel-injection system with dual shielded-magneto ignition. Power is transmitted via a 3-blade MT constant-speed (variable-pitch) propeller with spinner. The engine is supported by an oil cooler, exhaust muffler, engine-driven and auxiliary electric fuel pumps, and an electric starter. Fuel is carried in two integral tanks for 210 L total capacity, managed through a Left/Both/Right selector valve.

Avionics & Navigation. The aircraft is built around the Garmin G1000 NXi integrated flight deck, with dual 10″ GDU 1050 displays (PFD and MFD). Navigation and communication are handled by dual GIA 63W COM/NAV/GPS/GS/LOC units with WAAS, supported by a GRS 79 AHRS, GDC 72 air data computer, GMU 44 magnetometer and GTP 59 OAT probe. Audio is managed by a GMA 1347 digital audio system. A GTX 345R Mode-S transponder provides ADS-B In/Out, keeping the aircraft fully compliant for current and future airspace requirements. Redundancy is assured by an MD 302 standby attitude module and a lighted magnetic compass, with an ELT 406 Kannad and a full antenna suite (Marker Beacon, Transponder, VHF Com1 & Com2, NAV, ELT). A fully integrated two-axis GFC 700 Garmin autopilot is fitted, significantly reducing pilot workload on longer IFR legs.

Systems & Monitoring. Engine and airframe parameters are monitored by a dual GEA 71 unit, with comprehensive PFD annunciations (alternator, fuel pump, low fuel, low oil pressure, low voltage, pitot and rudder-trim status). Electrical power is supplied by a 28V/60A alternator and a 24V 8.0 Ah battery, with an external power receptacle and circuit-breaker panel. Safety equipment includes an audible stall warning and a cabin carbon-monoxide detection system.

Whether the goal is a cutting-edge glass-cockpit training platform or a capable, economical personal aircraft powered by Lycoming’s dependable IO-390, this 2024 P2010 stands out as one of the most advanced and cost-effective high-wing singles available today.