Tecnam P2010

Piston • single engine • High Wing • Fixed gear

Range Visualization

Origin: · click map to move · nm at current load

Payload vs. Range

Customize assumptions

Avg. pax weight (lbs)

Default: 190 lbs (FAA standard)

Luggage per pax (lbs)

Default: 30 lbs

Passengers

lbs @ lbs / pax

Select payload

0 lbs

Fuel on board

gal

+ Weight

Range

Available Range / nm

Mission capable — Aircraft can handle the current load with full fuel tanks.

Fuel tradeoff required — You'll need to leave gallons of fuel behind ( gal usable for nm range).

Over max gross weight — Reduce payload by lbs to safely operate this aircraft.

Mission Profile

140

KTAS

Cruise Speed

Occupants

720

Max Range

492

lbs

Wet Payload

Estimated Ownership Costs

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About the Tecnam P2010

The Tecnam P2010 is a modern four-seat aircraft that uniquely combines a carbon-fiber fuselage with metal wings. This high-wing design offers easy cabin access via three doors, spacious seating, and advanced Garmin avionics. With a 180 HP Lycoming engine, it provides a solid IFR-capable cross-country platform, balancing comfort, modern technology, and performance for personal owners and flight schools. For the luxury variant, see the Tecnam P2010 Gran Lusso