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)




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