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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

Range 720 nm
Cruise Speed 140 kt
Max Speed 140 kt

Specifications

ICAO Type CodeP201
Length25 ft 5 in
Wingspan / Rotor Diameter33 ft 11 in
Height8 ft 10 in
Empty Weight1687 lb
Max Takeoff Weight2557 lb
Cruise Speed140 kt
Max Speed140 kt
Range720 nm
Service Ceiling13000 ft
Engine ManufacturerLycoming / Continental
Engine ModelIO-360 / IO-390 / CD-170, variant-dependent
Engine Count1

Data verification status: Partially Verified

Source: Tecnam Aircraft - Aircraft Archive