Tecnam
Tecnam P2010
Four seats, carbon fuselage, certified.
View 2 photosThe P2010 is Tecnam's four-seat high-wing: carbon fuselage, metal wings, Lycoming 180 or 215 hp, and a cabin that competes with the Cessna 172 for schools and private owners who want something newer.
Key figures
Max speed
270 km/h
Range
1,400 km
Engine
Lycoming IO-360-L2A
Seats
4
Dimensions
Top view
Wingspan
10.3 m
Side view
Length
8 m
Height
2.6 m
Performance
Cruise
240 km/h
Max speed
270 km/h
Vne
292 km/h
Stall
90 km/h
Stall speed (clean)
101 km/h
Climb
5.5 m/s
Airframe
- Category
- Certified
- Wing
- High wing
- Seats
- 4
- Variant
- P2010
- First flight
- 2012
- Construction
- Carbon fuselage, metal wings
- Materials
- Carbon-fiber fuselage, aluminium wing
- Propeller
- MT or Hartzell
- Status
- in production
General
- ICAO type designator
P201
Likely · Tecnam P2010
- Propeller
Composite ground-adjustable, typical Rotax installation
Estimated · Manufacturer brochure / published figures
- Fuel
100LL / UL91
Likely · Manufacturer brochure / published figures
- Best glide ratio
11:1
Estimated · Manufacturer brochure / published figures
Weights
- Empty weight
760 kg
Likely · Tecnam P2010
- Max takeoff weight
1,160 kg
Likely · Tecnam P2010
- Useful load
400 kg
Estimated · Manufacturer brochure / published figures
- Fuel capacity
210 L
Likely · Tecnam P2010
Powerplant
- Propeller
Composite ground-adjustable, typical Rotax installation
Estimated · Manufacturer brochure / published figures
- Fuel
100LL / UL91
Likely · Manufacturer brochure / published figures