Tecnam P2008

Piston • single engine • High Wing • Fixed gear

Range Visualization

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

Payload vs. Range

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Default: 190 lbs (FAA standard)

Default: 30 lbs

Passengers
lbs @ lbs / pax
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

120
KTAS
Cruise Speed
2
Occupants
703
nm
Max Range
377
lbs
Wet Payload

Estimated Ownership Costs

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About the Tecnam P2008

The Tecnam P2008 is a modern, two-seat, high-wing aircraft designed for the Light Sport Aircraft (LSA) market, though certified variants like the P2008 JC exist. It is a desirable aircraft for General Aviation, especially for flight training and recreational flying, due to its blend of construction materials: a carbon-fiber fuselage combined with metal wings and a stabilator. This combination provides a comfortable cross-country ride and contributes to its relatively efficient operation. It features a spacious cabin, fixed tricycle landing gear, and is powered by a Rotax 912ULS piston engine, offering good fuel efficiency and low operating costs. Its practical ceiling is around 14,000 ft, and its range is suitable for touring.

Technical Specifications

Dimensions

Wingspan
29.5 ft
Length
22.87 ft
Height
8.76 ft

Weights

Max Takeoff Weight
1,433 lbs
Max Landing Weight
1,433 lbs
Useful Load
551 lbs
Fuel Capacity
29 gal

Performance

Cruise Speed
120 KTAS
Range
703 NM
Service Ceiling
14,000 ft
Rate of Climb
755 fpm

Engines

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