TYPE: Two-seat lightplane.

PROGRAMME: Introduced in 2002. Marketed in a range of roles, including flight training, pipeline patrol and agricultural applications.

DESIGN FEATURES: Braced high-wing monoplane with single strut each side. Sweptback fin.

FLYING CONTROLS: Conventional and manual. Electromechanical flaps.

STRUCTURE: Fuselage, wing and flying controls of glass fibre reinforced composites.

LANDING GEAR: Tricycle type; fixed. Fuselage-mounted spring metal cantilever mainwheel legs; telescopic, leaf-sprung nosewheel leg. Drum brakes. Optional floats and skis.

POWER PLANT: One 96.9 kW (130 hp) Limbach 2400 flat-four engine driving a wooden two-blade MT-Propeller MTV-1A/L170-05 propeller.

ACCOMMODATION: Two persons, side by side.

SYSTEMS: MVEN KC-700 ballistic parachute.

DIMENSIONS, EXTERNAL:

• Wing span: 10.12 m (33 ft 2½ in)
• Wing aspect ratio: 7.5
• Length overall: 6.63 m (21 ft 9 in)
• Height overall: 3.07 m (10 ft 0¾ in)
• Propeller diameter: 1.70 m (5 ft 7 in)

AREAS:

• Wings, gross: 13.66 m² (147.0 sq ft)

WEIGHTS AND LOADINGS:

• Weight empty: 540 kg (1,190 lb)
• Max T-O weight: 770 kg (1,697 lb)
• Max wing loading: 56,4 kg/m² (11.55 lb/sq ft)
• Max power loading: 7.95 kg/kW (13.06 lb/hp)

PERFORMANCE:

• Never exceed speed (V_NE): 124 kt (230 km/h; 142 mph)
• Max operating speed: 121 kt (224 km/h; 139 mph)
• Normal cruising speed: 86 kt (160 km/h; 99 mph)
• Stalling speed, flaps down: 46 kt (85 km/h; 53 mph)
• Mas rate of climb at S/L: 300 m (984 ft)/min
• Service ceiling: 3.500 m (11,480 ft)
• T-O run: 80 m (263 ft)
• Landing run: 90 m (295 ft)