Specifications .28204B.29 Bell 204/205
bell 204 rotor head bell 204 instrument panel data international directory of civil aircraft general characteristics crew: one-two capacity: 3,000 lb (1,360 kg) including eight-nine passengers, or equivalent cargo length: 41 ft 8 in (12.69 m) rotor diameter: 48 ft 0 in (14.63 m) height: 14 ft 7 in (4.5 m) disc area: 1,808 ft (168.0 m) empty weight: 4,600 lb (2,085 kg) useful load: lb (kg) loaded weight: lb (kg) max. takeoff weight: 9,500 lb (4,310 kg) powerplant: 1 × lycoming t53-l-11a turboshaft, 1,100 shp (820 kw) performance never exceed speed: knots (mph, km/h) maximum speed: 120 knots (135 mph, 220 km/h) cruise speed: 111 knots (125 mph, 205 km/h) stall speed: knots (mph, km/h) range: 300 nm (mi, 533 km) service ceiling: 19,390 ft (5,910 m) rate of climb: 1,755 ft/min (8.9 m/s) disc loading: lb/ft (kg/m) power/mass: hp/lb (w/kg) ^ cite error: named reference frawley civil invoked never defined (see page).