TYPE: Two-seat lightplane; side-by-side ultralight.
PROGRAMME: First flight 28 July 2000. Tailwheel version first shown at Berlin in May 2002, having achieved certification on 25 April 2002.
CURRENT VERSIONS: 100: Restricted weight and power to meet 450 kg (992 lb) limit.
130: Uprated version within US Experimental category limit. Prototype D-EKRK.
130TD: Tailwheel version introduced in 2002.
360: Higher-powered version; under development in 2002; to be certified under VLA requirements.
360TD: Tailwheel version of 360; under development. D-EEZZ shown unflown at Aero '03, Friedrichshafen in April 2003.
CUSTOMERS: Total 21 sold and 18 built by May 2002.
COSTS: Kit: 100 €46,400; 360 €48,500 less engine and interior; flyaway 100 €86,000; all excluding taxes (2003).
DESIGN FEATURES: Streamlined, low-wing configuration, with fuselage sharply waisted to rear of cockpit; laminar flow wing; sweptback fin with mid-mounted tailplane. Wide speed range. Available in Experimental and Ultralight weight categories. Quoted build time 450 hours; builder assistance programme available. Wings can be removed for storage and transportation.
FLYING CONTROLS: Conventional and manual. Horn-balanced rudder; flight-adjustable trim tab in port elevator. Electrically operated three-quarter-span Fowler flaps.
STRUCTURE: Fuselage of carbon-honeycomb sandwich with 1.7734.4 chromoloy engine mount. Wings of carbon-honeycomb sandwich with single main spar passing through fuselage under occupants' kness. Tail unit also of sandwich with E-glass fin, into which radio antennas are embedded. Aluminium main landing gear legs.
LANDING GEAR: Fixed tricycle or tailwheel (TD suffix) type with 5x5.00 mainwheels; tailwheel has solid 100 x 50 mm (4 x 2 in) type. Foam cushion shock dampeners. Hydraulic brakes.
POWER PLANT: 100: One 73.5 kW (98.6 hp) Rotax 912 S flat-four, driving an MT 167R152-2M wooden three-blade, variable-pitch propeller. Fuel in wing tanks, capacity 110 litres (29.1 US gallons; 24.2 Imp gallons). Option to fit 89.5 kW (120 hp) Jabiru 3300.
130 and 130TD: Options of 95 kW (128 hp) Limbach L2400ET flat-four and 118 kW (158 hp) LOM M332 in line four. Fuel capacity 160 litres (42.3 US gallons; 35.2 Imp gallons).
360 and 360TD: One 134 kW (180 hp) Textron Lycoming IO-360-M1A. Fuel capacity 200 litres (52.8 US gallons; 44.0 Imp gallons) in two integral wingtanks.
Optional power plants include BMW motorcycle engine and Thielert TAE 125 turbo-diesel.
ACCOMMODATION: Two persons, side by side, beneath single-piece hood; baggage space behind seats.
SYSTEMS: 12 V starter and generator.
EQUIPMENT: BRS parachute system.