Tecnam P2010
| Tecnam P2010 | |
|---|---|
|
|
| Type: | Light aircraft |
| Design country: | |
| Manufacturer: | |
| First flight: |
August 2012 |
The Tecnam P2010 is a single-engine, four-seat aircraft produced by the Italian manufacturer Tecnam .
construction
The stripped shoulder wing is made in a mixed construction of metal and fiber-reinforced plastic . The two wing tanks hold a total of 210 liters of AVGAS. A 132 kW (180 HP) Lycoming IO-360 -M1a piston engine serves as the engine . The tailplane is designed as a pendulum rudder, the wings have a trapezoidal base. The nose wheel is freely rotatable and is sprung by a rubber shock absorber. Asymmetrical braking is used when rolling on the ground.
The Tecnam P2010 will cost € 182,250.
Technical specifications
| Parameter | Tecnam P2010 |
|---|---|
| crew | 1 |
| Passengers | 3 |
| height | 2.64 m |
| length | 7.54 m |
| span | 10.50 m |
| Wing area | 14.60 m² |
| Tank capacity | 210 l |
| payload | 450 kg |
| Empty mass | 710 kg |
| Max. Takeoff mass | 1160 kg |
| Wing loading | 79.5 kg / m² |
| Cruising speed | 240 km / h (6500 ft, 75% power) |
| Rate of climb | 320 m / min |
| Engines | Lycoming IO-360 with 132 kW |
| Takeoff route | 245 m |
| Landing route | 200 m |
| Range | 1200 km (660 nm) |
Individual evidence
- ↑ Announcing the arrival of the TECNAM 'P2010'. In: tecnam.com. July 2010, archived from the original on October 26, 2010 ; accessed on September 16, 2011 .
- ↑ Tecnam P2010 - New litter from Professor Pascale. In: aerokurier.de. July 14, 2010, accessed September 16, 2011 .
- ↑ Tecnam four-seater P2010 - price correction. In: aerokurier.de. September 8, 2011, accessed September 16, 2011 .