DREAM AIRCRAFT TUNDRA

 

BRAND and MODEL
DREAM AIRCRAFT TUNDRA
TYPE
Four-seat light STOL utility monoplane
ORIGIN
Canada
ENGINE
One 150 kw (200 hp) Lycoming IO-360 four-cylinder horizontally-opposed air-cooled engine
SPECIFICATIONS

Wingspan: 10.97 m (36 ft)

Length: 7.77 m (25 ft 6 in)

Height: 2.13 m (7 ft 0 in)

Wing area: 17.06 m² (183.6 sq ft)

Never exceed speed: 259 km/h (161 mph)

Cruising speed at 75% power: 213 km/h (132 mph)

Stalling speed flaps down: 49 km/h (30 mph)

Rate of climb at sea level: 305 m/min (1,000 ft/min)

Service ceiling: 4,365 m (13,993 ft)

Range: 1,083 km (673 miles)

Take-off roll with wheels: 125 m (400 ft)

Take-off roll with floats: 200 m (650 ft)

Endurance: 5 hrs 12 mins

Empty weight: 658 kg (1,451 lb)

Loaded weight: 1,156 kg (2,549 lb)

PHOTO
planespotters.net:Source of phothograph