Specifications

Configuration

2 seater

Tailwheel

High wing monoplane

 

Dimensions

Length: 6.03 m (19.9 ft)

Wing span: 8.20 m (27 ft)

Wing chord: 1.225 m (4 ft)

Wing area: 10.06 sq. m (108.28 sq. ft)

Dihedral: 2 degrees

Cabin width: 106.68 cm (42 in)

Seat to roof skylight height: 93.98 cm (37 in)

Plenty of leg room for a 1.93 m (6 ft 4 in) pilot

Rudder pedals are adjustable

 

Propulsion system

Suitable engines: UL Power UL260, Simonini Victor 2 Super, Rotax 912, D-Motors LF26, Jabiru 2200/3300.

Fuel tanks capacity: 90 litresĀ (2×45 l wing tanks)

 

Weights

Empty weight: 310 Kg – varies with engine and equipment choice

Maximum Take off weight: 600 Kg

 

Performances

Maximum airspeed: 100 Kn (185 Km/h)

Stall airspeed 3 stage flaps: 36 to 45 Kn (67 to 83 Km/h)

Never Exceed Speed (Vne): 130 Kn (200 Km/h)

Fuel consumption: 12 – 18 liters/hour (depending on engine)

Endurance: 4.5 to 7 hrs with 10% reserve (depending on engine)

Rate of climb: 3.5 to 9 m/s (700 to 1800 ft/min) – dependant on engine and prop set up