BRAND and MODEL
BELL 204 And 205 (Civil Aircraft)
TYPE
Medium lift utility helicopter
ORIGIN
United States of America
ENGINE
One 820 kw (1,100 shp) Lycoming T53-L-11A turboshaft
SPECIFICATIONS
[204B]
Rotor diameter:14.63 m (48 ft)
Fuselage length:12.69 m (41 ft 8 in)
Overall length:17.4 m (57 ft 1½ in)
Height:4.5 m (14 ft 7 in)
Main rotor disc area:168 m² (1,808 sq ft)
Max speed at sea level:220 km/h (135 mph)
Max permissible diving speed:290 km/h (180 mph)
Max cruising speed:222 km/h (138 mph)
Economical cruising speed at 1,735 m (5,700 ft):204 km/h (127 mph)
Max rate of climb at sea level:535 m/min (1,760 ft/min)
Vertical rate of climb at sea level:340 m/min (1,115 ft/min)
Service ceiling:5,910 m (19,400 ft)
Hovering ceiling in ground effect:6,100 m (20,000 ft)
Hovering ceiling out of ground effect:4,750 m (15,600 ft)
Range with max fuel no allowances:526 km (327 miles)
Fuel capacity:832 litres (183 Imp gals)
Empty weight:2,085 kg (4,600 lb)
Loaded weight:4,309 kg (9,500 lb)
PHOTO
datuopinion.com:Source of phothograph
