Tecnam P2010
Overview
The Tecnam P2010 is a modern four-seat single-engine aircraft developed for personal transportation, touring and training roles. Tecnam lists current P2010 versions with multiple engine options, including gasoline and Jet-A/diesel configurations, and publishes cruise performance around 140 knots with maximum range figures up to roughly 1,300 nautical miles depending on version. Because the P2010 family includes materially different powerplants and operating weights, this encyclopedia entry should keep engine and performance values tied to the exact configuration being described. The aircraft is tracked as a distinct Tecnam type, with remaining blank specifications reserved for manufacturer or certification data rather than inferred from another P2010 version.
Quick Facts
Specifications
| ICAO Type Code | P201 |
|---|---|
| Length | 25 ft 5 in |
| Wingspan / Rotor Diameter | 33 ft 11 in |
| Height | 8 ft 10 in |
| Empty Weight | 1687 lb |
| Max Takeoff Weight | 2557 lb |
| Cruise Speed | 140 kt |
| Max Speed | 140 kt |
| Range | 720 nm |
| Service Ceiling | 13000 ft |
| Engine Manufacturer | Lycoming / Continental |
| Engine Model | IO-360 / IO-390 / CD-170, variant-dependent |
| Engine Count | 1 |
Data verification status: Partially Verified