Pilot, builder, owner Roger Jennings is singular in an uncommon way. He has built and loves to fly a Zenith CH-650 but he recently bought a used Tecnam P2008. You could say he goes both ways. Most of us, including your author, tend to fly only fully-built aircraft while another group of equal size enjoys the building process — or at least this is a more affordable path to airplane ownership. Roger truly enjoys his ‘650 on which he mounted a potent 130-horsepower Viking Aircraft Engines powerplant. “It climbs 2,000 feet per minute!” What red-blooded pilot can’t love that? The ‘650 is a low wing, however, and while Roger still loves it, his wife preferred a high wing. They’re easier to enter and offer some shade in Florida’s warm, sunny climate. World-Leading Tecnam After 18 years of Light-Sport Aircraft, Tecnam brand can claim to be the largest aircraft producer in this sector.
Flying Tecnam’s P2008 Turbo — Is a Used LSA Right for You?
World-Leading Tecnam
After 18 years of Light-Sport Aircraft, Tecnam brand can claim to be the largest aircraft producer in this sector. The Italian company has gone beyond LSA with a four seat, Part 23-certified aircraft (P2010) and an 11-seat commuter aircraft (P2012) yet the LSA sector remains vital to their enterprise. Numerically, they've sold many more of these than the higher end models.P2008 Description
P2008 is a conventional configuration, strut-braced high-wing design originally prepared for the American market. Learn more in the video below but Tecnam's P2008 differs from earlier models following their acquisition of a composite specialty company. Not long after, the Italian manufacturer mated a carbon fiber fuselage and tailplane to wings and control surfaces made of aluminum. P2008 is #106 on our SLSA List.Tecnam Aircraft P2008 (non-turbo) TECHNICAL SPECIFICATIONS all data supplied by the manufacturer
- Length — 22.87 feet (6,97 m)
- Height — 8.76 feet (2,67 m)
- Wingspan — 29.5 feet (9 m)
- Maximum Take Off Weight — 1,320 pounds (600 kg)
- Empty Weight, standard configuration — 827 pounds (375 kg)
- Useful Load — 496 pounds (225 kg)
- Baggage Capacity — 44 pounds (20 kg)
- Fuel Capacity — 32 U.S. gallons (123 lt)
- Max Cruise Speed — 128 knots (237 km/h)
- Stall Speed (flaps down, power off) — 39 knots 72 km/h
- Takeoff Roll — 600 feet (183 m)
- Landing Roll — 568 feet (173 m)
- Rate of Climb — 800 feet per minute (4,06 m/sec)
- Range — 514 nautical miles (952 km)
- Engine Manufacturer — Rotax 912ULS
- Engine Power — 100 horsepower
- Propeller — 2-blade fixed pitch
- Fuel Consumption — 4.5 gallons per hour (17 lt/h)
- Fuel Type — Mogas and Avgas