Dimensions

Wing span             .........      10.6 m (34 ft.)

Length                    .........       6.0 m (19 ft.)

Total height            .........      1.95 m

Wing area              .........      12.5 m2 (142 sq. ft.)

Wing slimness       .........       8.7 m

Wing depth            .........      1.2 m

Wing profile           .........       UA-2 and LS-1 / NASA

Cabin length          .........      1.2 m

Cabin width           .........      1 m

Cabin height         .........       0.95 m

Weights and loadings

Equipped empty    .........      225 kg

mtow                       .........      450 kg

Useful load             .........      225 kg

Usable fuel             .........       48 liter

Baggage                ….....       15 kg

Max. wing loading  ........    39.1 k/sq. m

g limits                    .........    +4/-2 g

Performance

Max. Speed (IAS) .........         162 kph

Max. cruise (IAS)   .........        140 kph

Economy cruise    .........         120 kph

Stall, full flap           ….....           45 kph

Range, no reserve ........ 250-350 miles

Climb s/l                 .........         500 fpm

Service ceiling       ........    12,000 ft

Take-off, ground roll .....            80 m

Landing, ground roll .....            70 m

Basic engine type:    

ROTAX 503 in-line twin air-cooled two-stroke, 

producing 52 HP at 6,000 rpm.

Prop 2,325 rpm, B reduction box, ratio 2.58:1

TBO: Rotax 503, 300 hours

Basic propeller type:

Junkers three blades carbon.

Diameter    ........      1600 mm