Write us a delivery method convenient for you – delivery of USB flash drives by mail or download files from Google Cloud!

By purchasing the product you will receive:
– plans and instructions,
– photos of the aircraft,
– video,
– a huge amount of useful information for building an airplane.

Delivery is free.

Thank you for your purchase.



The single seat Airbike was designed to meet the requirements of the United States FAR 103 Ultralight Vehicles, including the maximum 254 lb (115 kg) empty weight. The tandem-seat model was intended to be licensed as an ultralight trainer or an amateur-built aircraft.
The single-seater can achieve an empty weight as low as 251 lb (114 kg) with the use of a light-weight engine, such as the 28 hp (21 kW) Rotax 277 or the 22 hp (16 kW) Zenoah G-25.
The name Airbike was chosen for the aircraft because it has a narrow fuselage and the pilot’s feet rest on rudder pedals that are on the outside of the aircraft, in a similar manner to a motorcycle

General characteristics:

Crew: one
Capacity: no passengers
Length: 16 ft 0 in (4.88 m)
Wingspan: 26 ft 0 in (7.93 m)
Height: 5 ft 6 in (1.68 m)
Wing area: 118 sq ft (10.98 sq m)
Empty weight: 257 lb (116 kg)
Useful load: 303 lb (137 kg)
Max. takeoff weight: 560 lb (254 kg)
Powerplant: 1 × Rotax 447 fixed pitch, 40 hp (30 kW)
Propellers: 1 propeller, 1 per engine


Maximum speed: 80 mph (130 km/h)
Cruise speed: 63 mph (102 km/h)
Stall speed: 30 mph (49 km/h)
Range: 150 nautical miles (279 km)
Rate of climb: 1000 ft/min (5.1 m/s)
Wing loading: 4.75 lb/sq ft (23.1 kg/sq m)
Power/mass: 14 lb/hp (0.12 kW/kg)