TYPE: Side-by-side ultralight.

PROGRAMME: First flight 1995.

CUSTOMERS: Total 12 built by end of 1999; none known since, although promotion is continuing.

DESIGN FEATURES: Strut-braced high-wing cabin monoplane.

FLYING CONTROLS: Conventional and manual.

LANDING GEAR: Non-retractable tricycle type.

POWER PLANT: One 59.6 kW (79.9 hp) Rotax 912 UL or 47.8 kW (64.1 hp) Rotax 582 UL engine; three-blade propeller. Fuel capacity 35 litres (9.25 US gallons; 7.7 Imp gallons).

ACCOMMODATION: Door with large window each side.

DIMENSIONS, EXTERNAL:

• Wing span: 10.19 m (33 ft 5¼ in)
• Length overall: 5.70 m (18 ft 8½ in)
• Height overall: 2.37 m (7 ft 9¼ in)

AREAS:

• Wings, gross: 14.26 m² (153.5 sq ft)

WEIGHTS AND LOADINGS:

• Weight empty: 225 kg (496 lb)
• Max T-O weight: 450 kg (992 lb)

PERFORMANCE (Rotax 912 UL):

• Max level speed: 92 kt (170 km/h; 105 mph)
• Stalling speed: 36 kt (65 km/h; 41 mph)
• Max rate of climb at S/L: solo: 210 m (689 ft)/min
• two persons: 150 m (492 ft)/min
• Endurance: 4 h

The article appears in the following publication:
Jane's All the World's Aircraft 2004-2005. Jane's Information Group Ltd. 2004. ISBN: 0-7106-2614-2