the Italian challenger blends a carbon fiber fuselage with an all-metal wing, rudder, and stabilator, and offers specifications similar to those of the Cessna 172. The standard useful load of the P2010 is 992 pounds, better than the standard Cessna 172 useful load of 918 pounds. (The actual useful load of the P2010 flown at Tecnam’s United States headquarters in Sebring, Florida, is 910 pounds.) A new diesel engine option means even more possibilities for worldwide customers.
Lycoming IO-360-M1A, 180 hp
26 ft 2 in
8 ft 8 in
33 ft 9 in
3 ft 9 in
For more information, contact Tecnam Aircraft at or via https://www.tecnam.com/us/aircraft/p2010/
All specifications are based on manufacturer's calculations. All performance figures are based on standard day, standard atmosphere, sea level, gross weight conditions unless otherwise noted.