Height: 5 ft Width: 5.5 ft Length: 5 ft Structure: Carbon fibre composite Empty weight: 250 lbs (excluding safety equipment) Gross weight: 535 lbs Useful (Pilot) Load: 280 lbs+ Maximum thrust: 600 lbs+ Fuel Capacity: 5 US gallons (as required by FAA Part 103,Ultralight Regulations) Fuel burn: 10.0 gph Engine: Martin Aircraft 2.0 L V4 2 stroke, rated at 200 hp (150 kw). Max 6000 rpm. Electrical system: 12 V DC Battery, starter, 360 w alternator. Rotor: Carbon / Kevlar composite diameter 1.7 ft Max: 7058 rpm Range: 31.5 miles (at max speed of 63 mph as required by FAA part 103). Hover in ground effect: 8000 ft (estimated) Hover above ground effect: 8000 ft (estimated) Standard Equipment: Flight and Engine displays, Harness, Ballistic Parachute, Retractable undercarriage, Energy absorbing undercarriage. Classification: Meets the requirements of the FAA Part 103, Ultralight Regulations Pilot License: The Ultralight class does not require an FAA recognised pilots license.