Tecnam P2010
| P2010 | |
|---|---|
 |
|
| P2010 on display | |
| Role | Four seat light aircraft |
| National origin | Italy |
| Manufacturer | CostruzioniAeronautische Tecnam srl |
| First flight | 12 April 2012 |
| Produced | 2014–present |
| Number built | 25 (July 2014) |
| Unit cost |
US$345,000 (2015)
|
The Tecnam 2010 is a four-seat, high wing, single engine light aircraft of mixed metal and carbon-fiber-reinforced polymer construction. Designed and built in Italy, it was first presented in public in April 2011.
The Tecnam P2010 is a larger, four seat relative of the Tecnam P2008 two seat braced high wing light aircraft. Both types have metal wings and tailplane on a composite fuselage with integrated fin.
The wing leading edge is straight except for some pinching at the root and the wing has constant chord on the inner section. Outboard, the trailing edge is tapered; the straight wing tips are slightly upturned. Ailerons span the outboard panels and the inner sections carry flaps. There is a single lift strut on each side, attached to the lower fuselage. The P2010 has a low set all-moving constant chord tailplane with an anti-balance tab. The fin is swept and the rudder moves above the tailplane.
The P2010 is powered by a 135 kW (180 hp) Lycoming IO-360-M1A horizontally opposed four cylinder piston engine. The cabin seats the pilot and three passengers in two side-by-side rows, accessed by three doors. Its fixed tricycle undercarriage has spring cantilever main legs and a castoring nosewheel. All wheels have speed fairings.
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