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BRAND and MODEL
BOEING VERTOL 107
TYPE General purpose utility helicopter
ORIGIN United States of America
ENGINE Two 1,044 kw (1,400 shp) General Electric CT58-1040-1 turboshafts
SPECIFICATIONS
Rotor diameter: 15.24 m (50 ft)
Length rotors turning: 25.4 m (83 ft 4 in)
Height: 5.09 m (16 ft 8½ in)
Rotor disc area: 182.41 m² (1,963.5 sq ft)
Max speed at sea level: 254 km/h (158 mph)
Cruising speed at 1,525 m (5,000 ft): 241 km/h (150 mph)
Range with max fuel: 1,087 km (682 miles)
Empty weight: 5,251 kg (11,576 lb)
Loaded weight: 9,707 kg (21,400 lb)
PHOTO
Airliners.net:Source of phothograph
