Engine Lycoming IO-360-M1a
Basic empty weight 736,5 kg
Power 180HP Maximum take-off weight 1160 kg  
Fuel AVGAS 100LL Useful load 423,5 kg
Capacity of fuel in tanks 2 x 120 litres Overall height 2,64 m
Average fuel consumption 45 l/hour Overall lenght 7,97 m
Never exceed speed 166 KIAS Wing span 10,30 m
Maximum structural cruising speed 132 KIAS Number of pilots 1 – 2
Flight range 715 NM Number of passengers 3
Practical Ceiling 4572 m Number of aircraft in F AIR fleet 1


The Tecnam P Twenty-Ten brings together an advanced technology all carbon fibre fuselage with a metal wing to deliver a superlative single engined, 4 seat aeroplane, designed by Italy’s most innovative Aerospace design ‘guru’ Professor Luigi Pascale.

Powered by the well proven and reliable Lycoming IO-360-M1a (‘Lycoming Light’) engine, providing 180HP and 2700RPM. The Tecnam P Twenty-Ten has a high fuel capacity (240 litres). The fuel tanks are installed in the wing box, behind the main spar, to preserve their integrity in case of an accident. Of course carbon fibre equals a lighter and therefore more fuel efficient aeroplane.

Tecnam has always put the comfort for both pilots and passengers first. The Tecnam P Twenty-Ten with its spacious interior and its generous luggage compartment of 300 litres has been designed to be both a very enjoyable aeroplane to fly cross country as well as a robust trainer. The cabin width also allows for a large instrument panel, with its modular design specifically tailored to allow customers to fit digital instrumentation package, supermodern avionics GARMIN 1000.

Come to F AIR and get type rating for this new generation aircraft, Tecnam P2010 …