BRAND and MODEL
BELL 427
TYPE
General-purpose utility helicopter
ORIGIN
United States of America
ENGINE
Two 456 kw (611 shp) Pratt & Whitney Canada PW206D turboshafts
SPECIFICATIONS
Fuselage length: 10.94 m (35 ft 11 in)
Main rotor diameter: 11.28 m (37 ft)
Height: 3.9 m (12 ft 8 in)
Main rotor disc area: 99.9 m² (1,075.2 sq ft)
Max cruising speed at sea level: 252 km/h (157 mph)
Hovering ceiling in ground effect: 4,267 m (14,000 ft)
Hovering ceiling out of ground effect: 3,200 m (10,500 ft)
Range at sea level: 654 km (406 miles)
Fuel capacity: 720 litres (158 Imp gals)
Empty weight: 1,580 kg (3,485 lb)
Useful load: 1,135 kg (2,502 lb)
Loaded weight: 2,720 kg (6,000 lb)
PHOTO
Airliners.net:Source of phothograph
