TYPE: Light utility transport.

PROGRAMME: Incomplete fuselage exhibited at AirVenture, Oshkosh, July 2006; seeking partners to launch production.

CURRENT VERSIONS: Model 300: Baseline version: tailwheel; 224 kW (300 hp) Textron Lycoming IO-540 piston engine and short (11.73 m; 38 ft 5¾ in) wing span. MTOW 2,200 kg (4,850 lb); range 1,133 n miles (2,100 km; 1,304 miles) with 30 min reserves.
Model 400: As described.
Model 750 Turbo: With 559 kW (750 shp) Pratt & Whitney Canada PT6A turboprop. Otherwise generally as Model 400, except all-metal wing and eight fuel tanks, combined capacity 800 litres (211 US gallons; 176 Imp gallons); max level speed 170 kt (315 km/h; 196 mph); range 809 n miles (1,500 km; 932 miles); MTOW 2,700 kg (5,952 lb).

DESIGN FEATURES: Modelled on capabilities of DHC-2 Beaver. High, constant-chord, strut-braced wing; low, constant-chord tailplane; sweptback fin with small fillet. Landing gear, engine and wing area options.

FLYING CONTROLS: Conventional and manual.

STRUCTURE: Generally of metal, but fabric-covered wing (except metal for Model 750).

LANDING GEAR: Tricycle type; fixed. Telescopic mainwheel legs hinged to lower sides of fuselage and braced to centreline by V-type radius arms. Cantilever, trailing link nose unit. Model 300 has tailwheel and main leg attachments further forward. Optional floats and skis.

POWER PLANT: One 298 kW (400 hp) Textron Lycoming IO-720 piston engine. Fuel in six tanks, total capacity 432 litres (114 US gallons; 95.0 Imp gallons).

ACCOMMODATION: Seven persons, including one or two pilots. Two doors each side, separated by central window. Forward doors totally transparent.

Data follow for Model 400

DIMENSIONS, EXTERNAL:

  • Wing span: 13.575 m (44 ft 6½ in)
  • Wing aspect ratio: 7.4
  • Length overall: 11.075 m (36 ft 4 in)
  • Height overall: 3.885 (12 ft 9 in)

DIMENSIONS, INTERNAL:

  • Cabin: Length: 3.56 m (11 ft 8¼ in)
    • Max width: 1.38 m (4 ft 6¼ in)
    • Max height: 1.55 m (5 ft 1 in)

AREAS:

  • Wings, gross: 24.80 m² (266.9 sg ft)

WEIGHTS AND LOADINGS:

  • Max T-O weight: 2,300 kg (5,070 lb)
  • Max wing loading: 92.7 kg/m² (18.99 lb/sq ft)
  • Max power loading: 7.71 kg/kW (12.68 lb/hp)

PERFORMANCE:

  • Max level speed: 135 kt (250 km/h; 155 mph)
  • Stalling speed, flaps down: 38 kt (70 km/h; 44 mph)
  • T-O run: 48 m (160 ft)
  • T-O to 15 m (50 ft): 135 m (445 ft)
  • Landing from 15 m (50 ft): 162 m (535 ft)
  • Landing run: 42 m (140 ft)
  • Range with 30 min reserves: 1,133 n miles (2,100 km; 1,304 miles)