BRAND and MODEL
BELL 412
TYPE
Utility transport helicopter
ORIGIN
United States of America
ENGINE
One 1,343 kw (1,800 shp) (de-rated to 976 kw – 1,308 shp) Pratt & Whitney PT6T-3B-1 turbo twinpack turboshaft
SPECIFICATIONS
Rotor diameter: 14.02 m (46 ft)
Fuselage length: 12.7 m (41 ft 8½ in)
Height: 4.53 m (14 ft 10 in)
Main rotor disc area: 154.4 m² (1,662 sq ft)
Max speed at sea level: 240 km/h (149 mph)
Cruising speed at sea level: 230 km/h (143 mph)
Cruising speed at 1,525 m (5,000 ft): 235 km/h (146 mph)
Hovering ceiling in ground effect at 4,763 kg (10,500 lb): 3,290 m (10,800 ft)
Hovering ceiling out of ground effect: 2,165 m (7,100 ft)
Max range: 454 km (282 miles)
Range with auxiliary tanks: 834 km (518 miles)
Empty weight: 2,964 kg (6,535 lb)
Loaded weight: 5,397 kg (11,900 lb)
PHOTO
fotocommunity.de:Source of phothograph
