BRAND and MODEL
LAKE LA-270 SEAWOLF
TYPE
Five/six-seat amphibious utility aircraft
ORIGIN
United States of America
ENGINE
One 200 kw (270 hp) Textron Lycoming TIO-540-AA1AD six-cylinder horizontally-opposed air-cooled engine
SPECIFICATIONS
Wingspan: 11.58 m (38 ft)
Length: 8.64 m (28 ft 4 in)
Height: 3.05 m (10 ft)
Wing area: 15.8 m² (170 sq ft)
Cruising speed at 1,829 m (6,000 ft): 241 km/h (150 mph)
Cruising speed at 78% power at 6,096 m (20,000 ft): 286 km/h (178 mph)
Service ceiling: 4,480 m (14,700 ft)
Certified ceiling: 6,096 m (20,000 ft)
Rate of climb: 274 m/min (900 ft/min)
Range: 1,668 km (1,036 miles)
Take-off roll on land: 268 m (880 ft)
Take-off roll on water: 381 m (1,250 ft)
Landing roll on land: 145 m (475 ft)
Landing roll on water: 183 m (600 ft)
Empty weight: 941 kg (2,075 lb)
Useful load: 483 kg (1,065 lb)
Loaded weight: 1,424 kg (3,140 lb)
PHOTO
Airliners.net:Source of phothograph
