Tecnam P2010
The Tecnam 2010 is a four-seat, high wing, single engine light aircraft of mixed metal and carbon-fiber-reinforced polymer construction. Built and designed by Costruzioni Aeronautiche Tecnam, based in Capua, Italy, near Naples. The P2010 was first unveiled at the AERO Friedrichshafen show in April 2011 and made its maiden flight in 2012. It received type certification from the European Union Aviation Safety Agency (EASA) under CS-23 in September 2014, and FAA validation under FAR Part 23 followed in 2015. Developed from the two-seat Tecnam P2008, the P2010 introduced a larger carbon-fiber fuselage, all-metal wings, and Tecnam's signature all-moving stabilator. It was designed to offer modern ergonomics, a three-door cabin, and versatile engine options, including avgas and Jet-A capability.
Summary from Wikipedia, photo via Wikimedia Commons, licensed under CC BY-SA.
- Manufacturer
- Tecnam
- Category
- Single-engine piston
- Country of origin
- Italy
- First flight
- 2012-04-12
Specifications
- Cruise speed
- 128 kt
- Max speed
- 140 kt
- Range
- 960 nm
- Service ceiling
- 18,000 ft
- Rate of climb
- 1,420 ft/min
- Max takeoff weight
- 2,690 lb
- Empty weight
- 1,803 lb
- Fuel capacity
- 63.4 US gal
- Powerplant
- Continental CD-170
- Engines
- 1
- Seats
- 4
- Length
- 26.2 ft
- Wingspan
- 33.8 ft
- Height
- 8.7 ft
- Number built
- 245
Specifications are approximate and may vary by variant. Compiled from Wikipedia (CC BY-SA).
Reference and training only. Specifications vary by variant — consult the manufacturer and the official documents.